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 49081U 26145.38242120 +.00000000 +00000-0 +92112-4 0 00004
2 49081 87.9161 10.3965 0001810 96.7563 263.3774 13.17651919 01
| Epoch (UTC): | 25 May 2026 09:10:41 |
| Eccentricity: | 0.0001810 |
| inclination: | 87.9161° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3965° |
| argument of perigee: | 96.7563° |
| revolutions per day: | 13.17651919 |
| mean anomaly at epoch: | 263.3774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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