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 55657U 26145.48434266 +.00000000 +00000-0 +48371-4 0 00003
2 55657 69.9990 330.9890 0002967 266.7079 93.3741 14.98321637 06
| Epoch (UTC): | 25 May 2026 11:37:27 |
| Eccentricity: | 0.0002967 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.9890° |
| argument of perigee: | 266.7079° |
| revolutions per day: | 14.98321637 |
| mean anomaly at epoch: | 93.3741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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