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 56902U 26145.32092877 +.00000000 +00000-0 +19261-4 0 00004
2 56902 43.0060 358.2775 0000980 256.9863 103.0880 15.27577062 02
| Epoch (UTC): | 25 May 2026 07:42:08 |
| Eccentricity: | 0.0000980 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 358.2775° |
| argument of perigee: | 256.9863° |
| revolutions per day: | 15.27577062 |
| mean anomaly at epoch: | 103.0880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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