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 63723U 26145.58668372 +.00000000 +00000-0 +42787-3 0 00008
2 63723 53.1587 222.3189 0000574 112.6750 247.4312 15.30207850 01
| Epoch (UTC): | 25 May 2026 14:04:49 |
| Eccentricity: | 0.0000574 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.3189° |
| argument of perigee: | 112.6750° |
| revolutions per day: | 15.30207850 |
| mean anomaly at epoch: | 247.4312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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