LEOPARD, 67687
Orbit data source: Space-Track
LEOPARD, 67687 is a Japanese payload satellite in LEO that was delivered to the ISS. 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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67687 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
HUS
Mission
Operational spacecraft
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEOPARD
1 67687U 98067YD 26145.12106645 .00049348 00000-0 63782-3 0 9994
2 67687 51.6302 50.0450 0009759 97.5806 262.6296 15.58388834 16601Epoch: 2026-05-25T02:54Z
TLE epoch observation values (Epoch: 2026-05-25T02:54:20.141Z)
Latitude
0.00005°
Longitude
123.74771°
Altitude
393.916 km
Speed
7.675 km/s
True Right ascension
03h 20m 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
22:43:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
399.439 km
Perigee altitude
386.223 km
Semi-major axis
6,770.968 km
Eccentricity
0.00098
Inclination
51.6302°
RAAN
50.045°
Arg. of periapsis
97.5806°
True anomaly
262.51871°
Mean anomaly
262.6296°
Eccentric anomaly
262.57415°
Mean motion
3.89553 °/min
Orbital period
92.41 mins
BSTAR
0.00063782
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Other satellites on launch #67 in the year 1998 (1998-11-20 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.LEOPARD 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-25 20:00:46.903Z | 197.105° SSW | 2026-05-25 20:02:46.903Z | 137.064° SSE | 30.657° | 2026-05-25 20:04:46.903Z | 76.22° E |
| 4 mins | 2026-05-26 02:28:46.903Z | 333.154° NNW | 2026-05-26 02:29:46.903Z | 5.369° NNE | 33.209° | 2026-05-26 02:32:46.903Z | 104.469° ESE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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