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 56702U 26145.49633088 +.00000000 +00000-0 +36246-4 0 00007
2 56702 43.0017 204.2950 0001466 257.6316 102.4372 15.27577856 08
| Epoch (UTC): | 25 May 2026 11:54:42 |
| Eccentricity: | 0.0001466 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.2950° |
| argument of perigee: | 257.6316° |
| revolutions per day: | 15.27577856 |
| mean anomaly at epoch: | 102.4372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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