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 61960U 26145.25849953 +.00000000 +00000-0 +44989-3 0 00005
2 61960 43.0005 107.1103 0001031 250.8512 109.2228 15.27597340 04
| Epoch (UTC): | 25 May 2026 06:12:14 |
| Eccentricity: | 0.0001031 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.1103° |
| argument of perigee: | 250.8512° |
| revolutions per day: | 15.27597340 |
| mean anomaly at epoch: | 109.2228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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