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 29658U 06060A 26010.72489305 0.00009506 00000-0 34886-3 0 04
2 29658 98.1331 28.6706 0003982 55.7319 304.0874 15.27977831 04
| Epoch (UTC): | 10 January 2026 17:23:50 |
| Eccentricity: | 0.0003982 |
| inclination: | 98.1331° |
| perigee height: | 479 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 28.6706° |
| argument of perigee: | 55.7319° |
| revolutions per day: | 15.27977831 |
| mean anomaly at epoch: | 304.0874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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