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 26072.70123366 +.00000000 +00000-0 +24080-3 0 00008
2 29228 69.9324 226.6452 0001475 158.8768 201.2459 15.12776946 06
| Epoch (UTC): | 13 March 2026 16:49:46 |
| Eccentricity: | 0.0001475 |
| inclination: | 69.9324° |
| perigee height: | 527 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 226.6452° |
| argument of perigee: | 158.8768° |
| revolutions per day: | 15.12776946 |
| mean anomaly at epoch: | 201.2459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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