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 61729U 26145.15017638 +.00000000 +00000-0 -21749-4 0 00005
2 61729 53.1586 106.1398 0001756 93.7307 266.3895 15.30181690 04
| Epoch (UTC): | 25 May 2026 03:36:15 |
| Eccentricity: | 0.0001756 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.1398° |
| argument of perigee: | 93.7307° |
| revolutions per day: | 15.30181690 |
| mean anomaly at epoch: | 266.3895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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