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 62500U 26145.48603681 +.00000000 +00000-0 +60753-3 0 00004
2 62500 42.9993 215.5146 0001525 274.5468 85.5209 15.27593223 02
| Epoch (UTC): | 25 May 2026 11:39:53 |
| Eccentricity: | 0.0001525 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.5146° |
| argument of perigee: | 274.5468° |
| revolutions per day: | 15.27593223 |
| mean anomaly at epoch: | 85.5209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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