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 53057U 26145.43857069 +.00000000 +00000-0 -29859-3 0 00000
2 53057 97.4519 326.5597 0001565 184.7638 175.3575 15.05618534 09
| Epoch (UTC): | 25 May 2026 10:31:32 |
| Eccentricity: | 0.0001565 |
| inclination: | 97.4519° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5597° |
| argument of perigee: | 184.7638° |
| revolutions per day: | 15.05618534 |
| mean anomaly at epoch: | 175.3575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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