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 56461U 26145.42150212 +.00000000 +00000-0 +33661-4 0 00003
2 56461 69.9993 310.8273 0002957 267.7793 92.3027 14.98332079 06
| Epoch (UTC): | 25 May 2026 10:06:57 |
| Eccentricity: | 0.0002957 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.8273° |
| argument of perigee: | 267.7793° |
| revolutions per day: | 14.98332079 |
| mean anomaly at epoch: | 92.3027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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