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 Commercial Com/MetRO
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
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR-2 PEGGY-2004
1 68479U 26067BR 26263.11147194 .00002871 00000-0 27817-3 0 9998
2 68479 97.7646 220.1036 0001380 36.7492 323.3822 14.93491681 25895Epoch: 2026-09-20T02:40Z
TLE epoch observation values (Epoch: 2026-09-20T02:40:31.175Z)
Latitude
-0.00004°
Longitude
-179.03663°
Altitude
589.331 km
Speed
7.566 km/s
True Right ascension
14h 40m 24s
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
06:56:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.036 km
Perigee altitude
583.114 km
Semi-major axis
6,962.212 km
Eccentricity
0.00014
Inclination
97.7646°
RAAN
220.1036°
Arg. of periapsis
36.7492°
True anomaly
323.37277°
Mean anomaly
323.3822°
Eccentric anomaly
323.37748°
Mean motion
3.73613 °/min
Orbital period
96.36 mins
BSTAR
0.00027817
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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 | 2026-09-20 20:30:22.729Z | 121.196° SE | 2026-09-20 20:33:22.729Z | 65.216° ENE | 26.508° | 2026-09-20 20:36:22.729Z | 14.902° NNE |
| 5 mins | 2026-09-20 22:06:22.729Z | 222.914° SW | 2026-09-20 22:08:22.729Z | 259.695° W | 23.17° | 2026-09-20 22:11:22.729Z | 313.246° NW |
| 6 mins | 2026-09-21 09:48:22.729Z | 28.615° NE | 2026-09-21 09:51:22.729Z | 109.771° ESE | 51.327° | 2026-09-21 09:54:22.729Z | 173.182° S |
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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