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 61725U 26145.16703899 +.00000000 +00000-0 +32889-4 0 00009
2 61725 53.1608 106.2481 0001291 85.8748 274.2400 15.30196198 03
| Epoch (UTC): | 25 May 2026 04:00:32 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.2481° |
| argument of perigee: | 85.8748° |
| revolutions per day: | 15.30196198 |
| mean anomaly at epoch: | 274.2400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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