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 29107U 26150.51197727 +.00000000 +00000-0 +15861-3 0 00009
2 29107 98.3937 186.8224 0006014 41.4925 318.6744 14.86353477 08
| Epoch (UTC): | 30 May 2026 12:17:14 |
| Eccentricity: | 0.0006014 |
| inclination: | 98.3937° |
| perigee height: | 605 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 186.8224° |
| argument of perigee: | 41.4925° |
| revolutions per day: | 14.86353477 |
| mean anomaly at epoch: | 318.6744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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