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 55964U 26145.51406534 +.00000000 +00000-0 +78993-3 0 00007
2 55964 69.9963 63.7811 0005293 220.1248 139.9527 15.09742111 04
| Epoch (UTC): | 25 May 2026 12:20:15 |
| Eccentricity: | 0.0005293 |
| inclination: | 69.9963° |
| perigee height: | 533 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 63.7811° |
| argument of perigee: | 220.1248° |
| revolutions per day: | 15.09742111 |
| mean anomaly at epoch: | 139.9527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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