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, 0.3 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR-2 PEGGY-2004
1 68479U 26067BR 26217.41368439 .00003724 00000-0 36199-3 0 9998
2 68479 97.7571 174.9962 0003228 89.5387 270.6203 14.93184151 19079Epoch: 2026-08-05T09:55Z
TLE epoch observation values (Epoch: 2026-08-05T09:55:42.331Z)
Latitude
0.00005°
Longitude
72.10138°
Altitude
591.035 km
Speed
7.565 km/s
True Right ascension
11h 39m 59s
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
17:06:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.279 km
Perigee altitude
582.784 km
Semi-major axis
6,963.169 km
Eccentricity
0.00032
Inclination
97.7571°
RAAN
174.9962°
Arg. of periapsis
89.5387°
True anomaly
270.58331°
Mean anomaly
270.6203°
Eccentric anomaly
270.60181°
Mean motion
3.73536 °/min
Orbital period
96.38 mins
BSTAR
0.00036199
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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 | 2026-08-06 10:37:57.179Z | 344.016° N | 2026-08-06 10:39:57.179Z | 295.383° NW | 32.393° | 2026-08-06 10:43:57.179Z | 218.834° SW |
| 7 mins | 2026-08-06 21:25:57.179Z | 177.288° S | 2026-08-06 21:28:57.179Z | 224.981° SW | 41.621° | 2026-08-06 21:32:57.179Z | 340.974° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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