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 63807U 26145.36453138 +.00000000 +00000-0 +68251-3 0 00003
2 63807 42.9990 99.3017 0001519 269.5306 90.5372 15.27625254 00
| Epoch (UTC): | 25 May 2026 08:44:55 |
| Eccentricity: | 0.0001519 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.3017° |
| argument of perigee: | 269.5306° |
| revolutions per day: | 15.27625254 |
| mean anomaly at epoch: | 90.5372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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