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 56768U 26145.37353347 +.00000000 +00000-0 +70622-4 0 00009
2 56768 69.9989 130.9737 0003243 260.8490 99.2302 14.98331669 00
| Epoch (UTC): | 25 May 2026 08:57:53 |
| Eccentricity: | 0.0003243 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 130.9737° |
| argument of perigee: | 260.8490° |
| revolutions per day: | 14.98331669 |
| mean anomaly at epoch: | 99.2302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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