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 07727U 26044.32922288 +.00000000 +00000-0 +24846-4 0 00006
2 07727 65.5906 19.9387 0057204 187.1335 172.8930 13.99120052 01
| Epoch (UTC): | 13 February 2026 07:54:04 |
| Eccentricity: | 0.0057204 |
| inclination: | 65.5906° |
| perigee height: | 855 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 19.9387° |
| argument of perigee: | 187.1335° |
| revolutions per day: | 13.99120052 |
| mean anomaly at epoch: | 172.8930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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