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 53477U 26145.66668980 +.00000000 +00000-0 +34386-2 0 00002
2 53477 97.6024 267.7291 0001156 94.6033 136.8711 15.43272257 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001156 |
| inclination: | 97.6024° |
| perigee height: | 436 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 267.7291° |
| argument of perigee: | 94.6033° |
| revolutions per day: | 15.43272257 |
| mean anomaly at epoch: | 136.8711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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