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 10114U 26071.95619840 +.00000000 +00000-0 +32379-3 0 00005
2 10114 97.5779 244.0207 0006169 271.1830 88.8712 15.45596028 05
| Epoch (UTC): | 12 March 2026 22:56:55 |
| Eccentricity: | 0.0006169 |
| inclination: | 97.5779° |
| perigee height: | 425 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 244.0207° |
| argument of perigee: | 271.1830° |
| revolutions per day: | 15.45596028 |
| mean anomaly at epoch: | 88.8712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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