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 53482U 26145.28904510 +.00000000 +00000-0 -69372-4 0 00004
2 53482 97.4508 265.2783 0001576 179.1985 180.9245 15.05655929 05
| Epoch (UTC): | 25 May 2026 06:56:13 |
| Eccentricity: | 0.0001576 |
| inclination: | 97.4508° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 265.2783° |
| argument of perigee: | 179.1985° |
| revolutions per day: | 15.05655929 |
| mean anomaly at epoch: | 180.9245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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