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 63812U 26145.22092853 +.00000000 +00000-0 +67952-3 0 00004
2 63812 43.0010 99.9417 0001424 269.9752 90.0937 15.27597003 07
| Epoch (UTC): | 25 May 2026 05:18:08 |
| Eccentricity: | 0.0001424 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.9417° |
| argument of perigee: | 269.9752° |
| revolutions per day: | 15.27597003 |
| mean anomaly at epoch: | 90.0937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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