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 63465U 26145.57681076 +.00000000 +00000-0 +47181-3 0 00009
2 63465 43.0028 185.7312 0001988 277.5865 82.4761 15.27592646 01
| Epoch (UTC): | 25 May 2026 13:50:36 |
| Eccentricity: | 0.0001988 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7312° |
| argument of perigee: | 277.5865° |
| revolutions per day: | 15.27592646 |
| mean anomaly at epoch: | 82.4761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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