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 55051U 26145.52034471 +.00000000 +00000-0 +23531-3 0 00000
2 55051 97.5696 241.4664 0016498 93.5046 266.8080 15.28252307 07
| Epoch (UTC): | 25 May 2026 12:29:17 |
| Eccentricity: | 0.0016498 |
| inclination: | 97.5696° |
| perigee height: | 470 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 241.4664° |
| argument of perigee: | 93.5046° |
| revolutions per day: | 15.28252307 |
| mean anomaly at epoch: | 266.8080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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