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 56449U 26145.61346025 +.00000000 +00000-0 +63239-4 0 00003
2 56449 69.9981 310.6972 0003057 267.4899 92.5910 14.98332987 00
| Epoch (UTC): | 25 May 2026 14:43:22 |
| Eccentricity: | 0.0003057 |
| inclination: | 69.9981° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.6972° |
| argument of perigee: | 267.4899° |
| revolutions per day: | 14.98332987 |
| mean anomaly at epoch: | 92.5910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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