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 05707U 26020.22517846 +.00000000 +00000-0 +14371-3 0 00006
2 05707 74.0259 50.6210 0022669 71.3909 288.9705 14.40412973 00
| Epoch (UTC): | 20 January 2026 05:24:15 |
| Eccentricity: | 0.0022669 |
| inclination: | 74.0259° |
| perigee height: | 741 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 50.6210° |
| argument of perigee: | 71.3909° |
| revolutions per day: | 14.40412973 |
| mean anomaly at epoch: | 288.9705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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