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 63572U 26145.56530662 +.00000000 +00000-0 +65226-3 0 00001
2 63572 42.9977 247.8832 0001154 277.9000 82.1720 15.27597263 00
| Epoch (UTC): | 25 May 2026 13:34:02 |
| Eccentricity: | 0.0001154 |
| inclination: | 42.9977° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.8832° |
| argument of perigee: | 277.9000° |
| revolutions per day: | 15.27597263 |
| mean anomaly at epoch: | 82.1720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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