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 29228U 26158.97910051 +.00000000 +00000-0 +16340-3 0 00007
2 29228 69.9339 3.3886 0006437 299.3252 60.7270 15.13177297 09
| Epoch (UTC): | 07 June 2026 23:29:54 |
| Eccentricity: | 0.0006437 |
| inclination: | 69.9339° |
| perigee height: | 522 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 3.3886° |
| argument of perigee: | 299.3252° |
| revolutions per day: | 15.13177297 |
| mean anomaly at epoch: | 60.7270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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