LACE-1, 59118 (Decayed)
Orbit data source: Space-Track
LACE-1, 59118 was a payload satellite owned by NIWC Pacific (US) in LEO that was launched on Mon, 04 Mar 2024 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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59118 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
PUMPK/NIWCP
Mission
Decayed Defense Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 LACE-1
1 59118U 24043W 25138.97701806 .11616415 26017-5 59933-3 0 9992
2 59118 97.4688 279.1037 0013725 262.2912 97.6829 16.41284763 67656Epoch: 2025-05-18T23:26Z
TLE epoch observation values (Epoch: 2025-05-18T23:26:54.360Z)
Latitude
-0.00006°
Longitude
50.48096°
Altitude
166.851 km
Speed
7.805 km/s
True Right ascension
18h 36m 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
13:37:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
168.169 km
Perigee altitude
150.224 km
Semi-major axis
6,537.333 km
Eccentricity
0.00137
Inclination
97.4688°
RAAN
279.1037°
Arg. of periapsis
262.2912°
True anomaly
97.83873°
Mean anomaly
97.6829°
Eccentric anomaly
97.76082°
Mean motion
4.10622 °/min
Orbital period
87.67 mins
BSTAR
0.00059933
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.LACE-1 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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