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 56772U 26145.36981536 +.00000000 +00000-0 +14173-4 0 00009
2 56772 69.9984 171.0931 0003917 267.3988 92.6723 14.98331622 07
| Epoch (UTC): | 25 May 2026 08:52:32 |
| Eccentricity: | 0.0003917 |
| inclination: | 69.9984° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 171.0931° |
| argument of perigee: | 267.3988° |
| revolutions per day: | 14.98331622 |
| mean anomaly at epoch: | 92.6723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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