NASA will be performing network maintenance on Wednesday, Thursday, December 5, 2024, between 9:00 AM EST and 11:00 AM EST (14:00 to 16:00 UTC). There will be two periods of about five minutes of disruption. During these peroids, the ILRS website will be unavailable during the outages. If you experience problems outside this window, contact support-cddis@nasa.gov.

close window
general navigation structure general satellite info ilrs support retroreflector info center of mass site performance info

RANGE

Jump to: Mission Objectives, Mission Instrumentation, Mission Parameters, Additional Information

Mission Photos:

RANGE satellites
Courtesy of Georgia Institute of Technology

Mission Objectives:

RANGE (The Ranging And Nanosatellite Guidance Experiment) is a cubesat mission consisting of two satellites in a leader-follower formation. The primary objective of the mission is to improve the relative and absolute positioning capabilities of small satellites. This will be done through ground-based laser ranging, a dual-frequency GPS receiver, and an intersatellite laser ranging system (operating at 1550 nm). The goal is to achieve cm-level absolute positioning and mm-level relative positioning knowledge.

SLR will be used together with the positioning information gathered from the on-board GPS receivers and intersatellite ranging system for precise orbit determination. The nadir-pointing side of each RANGE spacecraft has four retroreflectors for increased field-of-view, in addition to a fifth pop-out retroreflector on one side for attitude determination experiments.

RANGE Mission Parameters:
Satellite RANGE (satellite A) RANGE (satellite B)
Sponsor: Georgia Institute of Technology Georgia Institute of Technology
Expected Life: 1 year 1 year
Primary Applications: Improve the relative and absolute positioning capabilities of small satellites Improve the relative and absolute positioning capabilities of small satellites
Primary SLR Application: Precision orbit determination Precision orbit determination
Launch Date: July/Aug 2018 July/Aug 2018
COSPAR ID:    
SIC: 1077 1078
Satellite Catalog (NORAD)
Number:
   
NP Bin Size: 15 seconds 15 seconds
RRA Diameter:    
RRA Shape: 4 Nadir Canted Pyramid and 1 Nadir Canted on Flip-Out Mount 4 Nadir Canted Pyramid and 1 Nadir Canted on Flip-Out Mount
Reflectors: 5 5
Orbit:    
Inclination: 97.7 degrees 97.7 degrees
Eccentricity: 0 degrees 0 degrees
Altitude: 575 km 575 km
Period: 5770 sec (96.2 min) 5770 sec (96.2 min)
Additional Information:

Web sites: