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 53229U 26145.44684457 +.00000000 +00000-0 -12741-3 0 00003
2 53229 97.4475 206.4821 0002241 120.2388 239.9061 15.05660856 07
| Epoch (UTC): | 25 May 2026 10:43:27 |
| Eccentricity: | 0.0002241 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4821° |
| argument of perigee: | 120.2388° |
| revolutions per day: | 15.05660856 |
| mean anomaly at epoch: | 239.9061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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