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 63815U 26145.16453824 +.00000000 +00000-0 +62094-3 0 00001
2 63815 43.0001 100.3830 0001586 276.6026 83.4646 15.27587129 05
| Epoch (UTC): | 25 May 2026 03:56:56 |
| Eccentricity: | 0.0001586 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.3830° |
| argument of perigee: | 276.6026° |
| revolutions per day: | 15.27587129 |
| mean anomaly at epoch: | 83.4646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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