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 05681U 26032.14701185 +.00000000 +00000-0 +72738-4 0 00004
2 05681 69.9890 286.5590 0009373 325.3311 34.7171 13.74629215 01
| Epoch (UTC): | 01 February 2026 03:31:41 |
| Eccentricity: | 0.0009373 |
| inclination: | 69.9890° |
| perigee height: | 976 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 286.5590° |
| argument of perigee: | 325.3311° |
| revolutions per day: | 13.74629215 |
| mean anomaly at epoch: | 34.7171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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