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 55269U 26145.46207943 +.00000000 +00000-0 -62081-5 0 00006
2 55269 69.9989 210.9646 0003815 267.4917 92.5805 14.98336237 05
| Epoch (UTC): | 25 May 2026 11:05:23 |
| Eccentricity: | 0.0003815 |
| inclination: | 69.9989° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 210.9646° |
| argument of perigee: | 267.4917° |
| revolutions per day: | 14.98336237 |
| mean anomaly at epoch: | 92.5805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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