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 26076.13340247 +.00000000 +00000-0 +84580-4 0 00006
2 05707 74.0268 307.1857 0024625 313.8147 46.0971 14.40459095 03
| Epoch (UTC): | 17 March 2026 03:12:05 |
| Eccentricity: | 0.0024625 |
| inclination: | 74.0268° |
| perigee height: | 739 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 307.1857° |
| argument of perigee: | 313.8147° |
| revolutions per day: | 14.40459095 |
| mean anomaly at epoch: | 46.0971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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