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 49091U 26145.50846442 +.00000000 +00000-0 +39973-3 0 00001
2 49091 87.8961 355.1763 0001575 94.6721 265.4587 13.12440512 01
| Epoch (UTC): | 25 May 2026 12:12:11 |
| Eccentricity: | 0.0001575 |
| inclination: | 87.8961° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1763° |
| argument of perigee: | 94.6721° |
| revolutions per day: | 13.12440512 |
| mean anomaly at epoch: | 265.4587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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