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 53212U 26145.40254081 +.00000000 +00000-0 -16796-3 0 00001
2 53212 97.4483 206.4560 0002142 106.4773 253.6690 15.05664460 08
| Epoch (UTC): | 25 May 2026 09:39:39 |
| Eccentricity: | 0.0002142 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4560° |
| argument of perigee: | 106.4773° |
| revolutions per day: | 15.05664460 |
| mean anomaly at epoch: | 253.6690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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