LEMUR-2 PEGGY-2004, 68479
Orbit data source: Space-Track
LEMUR-2 PEGGY-2004, 68479 is a payload satellite owned by Spire (LU) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68479 intel report (Beta)
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Identifier
Orbit
Country
LU / LUXERelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 LEMUR-2 PEGGY-2004
1 68479U 26067BR 26153.80662751 .00007003 00000-0 68641-3 0 9995
2 68479 97.7539 112.2957 0001217 37.5275 322.6029 14.92553604 9588Epoch: 2026-06-02T19:21Z
TLE epoch observation values (Epoch: 2026-06-02T19:21:32.616Z)
Latitude
-0.00005°
Longitude
-69.3645°
Altitude
592.346 km
Speed
7.564 km/s
True Right ascension
07h 29m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:18:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.842 km
Perigee altitude
586.146 km
Semi-major axis
6,965.131 km
Eccentricity
0.00012
Inclination
97.7539°
RAAN
112.2957°
Arg. of periapsis
37.5275°
True anomaly
322.59443°
Mean anomaly
322.6029°
Eccentric anomaly
322.59866°
Mean motion
3.73378 °/min
Orbital period
96.42 mins
BSTAR
0.00068641
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR-2 PEGGY-2004 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-06 21:38:32.754Z | 196.191° SSW | 2026-06-06 21:40:32.754Z | 245.566° WSW | 36.082° | 2026-06-06 21:44:32.754Z | 334.47° NNW |
| 5 mins | 2026-06-07 09:21:32.754Z | 51.216° ENE | 2026-06-07 09:23:32.754Z | 88.839° E | 22.837° | 2026-06-07 09:26:32.754Z | 145.223° SSE |
| 5 mins | 2026-06-07 10:57:32.754Z | 326.275° NNW | 2026-06-07 10:59:32.754Z | 283.656° WNW | 22.525° | 2026-06-07 11:02:32.754Z | 236.685° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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