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 62572U 26145.49572247 +.00000000 +00000-0 +49573-3 0 00004
2 62572 42.9989 218.4173 0001023 271.4595 88.6139 15.27592544 09
| Epoch (UTC): | 25 May 2026 11:53:50 |
| Eccentricity: | 0.0001023 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 218.4173° |
| argument of perigee: | 271.4595° |
| revolutions per day: | 15.27592544 |
| mean anomaly at epoch: | 88.6139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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