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 49113U 26145.63698049 +.00000000 +00000-0 +14820-3 0 00002
2 49113 86.4016 92.0633 0017514 279.7694 80.1510 14.09458268 02
| Epoch (UTC): | 25 May 2026 15:17:15 |
| Eccentricity: | 0.0017514 |
| inclination: | 86.4016° |
| perigee height: | 849 km |
| apogee height: | 874 km |
| right ascension of ascending node: | 92.0633° |
| argument of perigee: | 279.7694° |
| revolutions per day: | 14.09458268 |
| mean anomaly at epoch: | 80.1510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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