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 55963U 26145.52721365 +.00000000 +00000-0 +31284-5 0 00003
2 55963 70.0005 70.6874 0002960 262.3991 97.6832 14.98330220 00
| Epoch (UTC): | 25 May 2026 12:39:11 |
| Eccentricity: | 0.0002960 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.6874° |
| argument of perigee: | 262.3991° |
| revolutions per day: | 14.98330220 |
| mean anomaly at epoch: | 97.6832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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