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 49213U 26145.38644773 +.00000000 +00000-0 +20017-3 0 00005
2 49213 87.9178 278.9861 0002311 108.7921 251.3463 13.20770262 01
| Epoch (UTC): | 25 May 2026 09:16:29 |
| Eccentricity: | 0.0002311 |
| inclination: | 87.9178° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9861° |
| argument of perigee: | 108.7921° |
| revolutions per day: | 13.20770262 |
| mean anomaly at epoch: | 251.3463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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