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 26070.84979438 +.00000000 +00000-0 +20973-3 0 00007
2 29228 69.9325 231.4346 0001684 161.0804 199.0425 15.12761411 00
| Epoch (UTC): | 11 March 2026 20:23:42 |
| Eccentricity: | 0.0001684 |
| inclination: | 69.9325° |
| perigee height: | 527 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 231.4346° |
| argument of perigee: | 161.0804° |
| revolutions per day: | 15.12761411 |
| mean anomaly at epoch: | 199.0425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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