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 61229U 26145.59999073 +.00000000 +00000-0 +57572-3 0 00001
2 61229 97.3413 227.8661 0011065 215.6253 144.4260 15.47895140 03
| Epoch (UTC): | 25 May 2026 14:23:59 |
| Eccentricity: | 0.0011065 |
| inclination: | 97.3413° |
| perigee height: | 415 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 227.8661° |
| argument of perigee: | 215.6253° |
| revolutions per day: | 15.47895140 |
| mean anomaly at epoch: | 144.4260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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