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 62573U 26145.50600854 +.00000000 +00000-0 +56191-3 0 00007
2 62573 42.9975 218.4987 0001067 280.8453 79.2278 15.27611439 08
| Epoch (UTC): | 25 May 2026 12:08:39 |
| Eccentricity: | 0.0001067 |
| inclination: | 42.9975° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 218.4987° |
| argument of perigee: | 280.8453° |
| revolutions per day: | 15.27611439 |
| mean anomaly at epoch: | 79.2278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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