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 53056U 26145.48008566 +.00000000 +00000-0 +68631-3 0 00004
2 53056 97.4452 326.5195 0001790 141.1721 218.9635 15.05602320 05
| Epoch (UTC): | 25 May 2026 11:31:19 |
| Eccentricity: | 0.0001790 |
| inclination: | 97.4452° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5195° |
| argument of perigee: | 141.1721° |
| revolutions per day: | 15.05602320 |
| mean anomaly at epoch: | 218.9635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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