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 26088.13944237 +.00000000 +00000-0 +37598-3 0 00002
2 10114 97.5793 260.9278 0006781 203.9986 156.0948 15.46044970 05
| Epoch (UTC): | 29 March 2026 03:20:47 |
| Eccentricity: | 0.0006781 |
| inclination: | 97.5793° |
| perigee height: | 424 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 260.9278° |
| argument of perigee: | 203.9986° |
| revolutions per day: | 15.46044970 |
| mean anomaly at epoch: | 156.0948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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