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 62510U 26145.53343409 +.00000000 +00000-0 +53101-3 0 00009
2 62510 42.9989 215.0097 0001678 262.7299 97.3362 15.27587636 00
| Epoch (UTC): | 25 May 2026 12:48:08 |
| Eccentricity: | 0.0001678 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.0097° |
| argument of perigee: | 262.7299° |
| revolutions per day: | 15.27587636 |
| mean anomaly at epoch: | 97.3362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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