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 26019.29377801 +.00000000 +00000-0 +29577-3 0 00008
2 10114 97.5702 189.1180 0008584 100.0210 260.2006 15.43947601 02
| Epoch (UTC): | 19 January 2026 07:03:02 |
| Eccentricity: | 0.0008584 |
| inclination: | 97.5702° |
| perigee height: | 429 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 189.1180° |
| argument of perigee: | 100.0210° |
| revolutions per day: | 15.43947601 |
| mean anomaly at epoch: | 260.2006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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