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 49311U 26145.33595336 +.00000000 +00000-0 +29300-3 0 00003
2 49311 87.9174 278.9960 0002074 96.9586 263.1783 13.20767563 03
| Epoch (UTC): | 25 May 2026 08:03:46 |
| Eccentricity: | 0.0002074 |
| inclination: | 87.9174° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9960° |
| argument of perigee: | 96.9586° |
| revolutions per day: | 13.20767563 |
| mean anomaly at epoch: | 263.1783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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