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 63972U 26145.55434719 +.00000000 +00000-0 +36458-3 0 00005
2 63972 42.9974 98.4971 0001029 263.4320 96.6415 15.27588860 05
| Epoch (UTC): | 25 May 2026 13:18:15 |
| Eccentricity: | 0.0001029 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.4971° |
| argument of perigee: | 263.4320° |
| revolutions per day: | 15.27588860 |
| mean anomaly at epoch: | 96.6415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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