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 54700U 26145.64662288 +.00000000 +00000-0 +63961-4 0 00008
2 54700 59.9977 315.0061 0013392 182.8916 177.2044 14.29532939 05
| Epoch (UTC): | 25 May 2026 15:31:08 |
| Eccentricity: | 0.0013392 |
| inclination: | 59.9977° |
| perigee height: | 784 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 315.0061° |
| argument of perigee: | 182.8916° |
| revolutions per day: | 14.29532939 |
| mean anomaly at epoch: | 177.2044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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