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 00705U 26053.83330068 +.00000000 +00000-0 +85016-4 0 00006
2 00705 89.9153 71.3128 0032453 221.6189 260.1868 13.47658239 06
| Epoch (UTC): | 22 February 2026 19:59:57 |
| Eccentricity: | 0.0032453 |
| inclination: | 89.9153° |
| perigee height: | 1057 km |
| apogee height: | 1105 km |
| right ascension of ascending node: | 71.3128° |
| argument of perigee: | 221.6189° |
| revolutions per day: | 13.47658239 |
| mean anomaly at epoch: | 260.1868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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