View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63816U 26145.14412484 +.00000000 +00000-0 +50335-3 0 00002
2 63816 43.0007 101.0920 0001395 272.1856 87.8836 15.27589587 09
| Epoch (UTC): | 25 May 2026 03:27:32 |
| Eccentricity: | 0.0001395 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 101.0920° |
| argument of perigee: | 272.1856° |
| revolutions per day: | 15.27589587 |
| mean anomaly at epoch: | 87.8836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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