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 63845U 26145.62386354 +.00000000 +00000-0 -18490-3 0 00000
2 63845 42.9976 3.8223 0001537 272.9993 87.0683 15.27568065 07
| Epoch (UTC): | 25 May 2026 14:58:21 |
| Eccentricity: | 0.0001537 |
| inclination: | 42.9976° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.8223° |
| argument of perigee: | 272.9993° |
| revolutions per day: | 15.27568065 |
| mean anomaly at epoch: | 87.0683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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