ICOR SV, 68127 (Decayed)
Orbit data source: Space-Track
ICOR SV, 68127 was a payload satellite owned by LMSS Denver (US) in LEO that was launched on Thu, 12 Mar 2026 UTC via an FIREFLY ALPHA 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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68127 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LMSS Denver
Mission
Decayed spacecraft
Bus & Motor
LM-400, Unknown motor
Mass
~1,100 kg wet, ~1,100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 ICOR SV
1 68127U 26046A 26109.59295808 .02873854 13124-4 51214-3 0 9994
2 68127 123.0635 36.1737 0038563 269.9104 89.7570 16.29449949 6143Epoch: 2026-04-19T14:13Z
TLE epoch observation values (Epoch: 2026-04-19T14:13:51.578Z)
Latitude
0°
Longitude
-24.98643°
Altitude
195.361 km
Speed
7.79 km/s
True Right ascension
02h 24m 41s
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
08:33:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
219.007 km
Perigee altitude
168.321 km
Semi-major axis
6,571.801 km
Eccentricity
0.00386
Inclination
123.0635°
RAAN
36.1737°
Arg. of periapsis
269.9104°
True anomaly
90.1989°
Mean anomaly
89.757°
Eccentric anomaly
89.97795°
Mean motion
4.07396 °/min
Orbital period
88.37 mins
BSTAR
0.00051214
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Other satellites on launch #46 in the year 2026 (2026-03-12 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.ICOR SV Visibility
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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. |
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| This satellite is decayed. |
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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