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 26062.91484493 +.00000000 +00000-0 +21006-3 0 00006
2 29228 69.9304 251.9622 0002432 165.6205 194.5031 15.12697372 05
| Epoch (UTC): | 03 March 2026 21:57:22 |
| Eccentricity: | 0.0002432 |
| inclination: | 69.9304° |
| perigee height: | 526 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 251.9622° |
| argument of perigee: | 165.6205° |
| revolutions per day: | 15.12697372 |
| mean anomaly at epoch: | 194.5031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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