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 66403U 26145.48724171 +.00000000 +00000-0 +50807-3 0 00007
2 66403 53.1588 219.4453 0001205 80.5639 279.5500 15.34395880 02
| Epoch (UTC): | 25 May 2026 11:41:37 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 219.4453° |
| argument of perigee: | 80.5639° |
| revolutions per day: | 15.34395880 |
| mean anomaly at epoch: | 279.5500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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