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 49160U 26145.31684983 +.00000000 +00000-0 -23981-4 0 00001
2 49160 69.9995 101.2347 0003406 260.3955 99.6819 14.98335830 06
| Epoch (UTC): | 25 May 2026 07:36:15 |
| Eccentricity: | 0.0003406 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 101.2347° |
| argument of perigee: | 260.3955° |
| revolutions per day: | 14.98335830 |
| mean anomaly at epoch: | 99.6819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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