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 63813U 26145.55219209 +.00000000 +00000-0 +10186-2 0 00003
2 63813 43.0013 94.6212 0001391 258.1121 101.9575 15.27585325 03
| Epoch (UTC): | 25 May 2026 13:15:09 |
| Eccentricity: | 0.0001391 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 94.6212° |
| argument of perigee: | 258.1121° |
| revolutions per day: | 15.27585325 |
| mean anomaly at epoch: | 101.9575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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