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 53485U 26145.29180596 +.00000000 +00000-0 -10073-3 0 00001
2 53485 97.4466 265.2578 0001255 154.2363 205.8927 15.05663561 06
| Epoch (UTC): | 25 May 2026 07:00:12 |
| Eccentricity: | 0.0001255 |
| inclination: | 97.4466° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.2578° |
| argument of perigee: | 154.2363° |
| revolutions per day: | 15.05663561 |
| mean anomaly at epoch: | 205.8927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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