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 29517U 26039.13426220 +.00000000 +00000-0 +15760-3 0 00009
2 29517 28.2495 285.8164 4052508 344.9941 5.8602 6.89890249 04
| Epoch (UTC): | 08 February 2026 03:13:20 |
| Eccentricity: | 0.4052508 |
| inclination: | 28.2495° |
| perigee height: | 554 km |
| apogee height: | 10001 km |
| right ascension of ascending node: | 285.8164° |
| argument of perigee: | 344.9941° |
| revolutions per day: | 6.89890249 |
| mean anomaly at epoch: | 5.8602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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