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 05816U 26041.22019046 +.00000000 +00000-0 -48380-3 0 00007
2 05816 28.5966 357.8399 7185434 195.5879 141.3300 2.20981220 06
| Epoch (UTC): | 10 February 2026 05:17:04 |
| Eccentricity: | 0.7185434 |
| inclination: | 28.5966° |
| perigee height: | 630 km |
| apogee height: | 36410 km |
| right ascension of ascending node: | 357.8399° |
| argument of perigee: | 195.5879° |
| revolutions per day: | 2.20981220 |
| mean anomaly at epoch: | 141.3300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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