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 63634U 26145.45856541 +.00000000 +00000-0 +55946-3 0 00003
2 63634 42.9998 292.0102 0001473 267.7363 92.3320 15.27590025 05
| Epoch (UTC): | 25 May 2026 11:00:20 |
| Eccentricity: | 0.0001473 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 292.0102° |
| argument of perigee: | 267.7363° |
| revolutions per day: | 15.27590025 |
| mean anomaly at epoch: | 92.3320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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