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 07714U 26088.11285229 +.00000000 +00000-0 +47875-4 0 00001
2 07714 81.1914 307.7146 0029430 216.2231 143.6947 14.08465565 06
| Epoch (UTC): | 29 March 2026 02:42:30 |
| Eccentricity: | 0.0029430 |
| inclination: | 81.1914° |
| perigee height: | 843 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 307.7146° |
| argument of perigee: | 216.2231° |
| revolutions per day: | 14.08465565 |
| mean anomaly at epoch: | 143.6947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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