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 45229U 26145.31714581 +.00000000 +00000-0 +11963-2 0 00005
2 45229 53.1587 358.6136 0002690 158.5721 201.5398 15.42311065 07
| Epoch (UTC): | 25 May 2026 07:36:41 |
| Eccentricity: | 0.0002690 |
| inclination: | 53.1587° |
| perigee height: | 437 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 358.6136° |
| argument of perigee: | 158.5721° |
| revolutions per day: | 15.42311065 |
| mean anomaly at epoch: | 201.5398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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