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 53232U 26145.40672272 +.00000000 +00000-0 +20549-4 0 00000
2 53232 97.4504 205.3137 0000991 155.2599 204.8676 15.05649375 00
| Epoch (UTC): | 25 May 2026 09:45:40 |
| Eccentricity: | 0.0000991 |
| inclination: | 97.4504° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.3137° |
| argument of perigee: | 155.2599° |
| revolutions per day: | 15.05649375 |
| mean anomaly at epoch: | 204.8676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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