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 55286U 26145.57033409 +.00000000 +00000-0 +23901-5 0 00008
2 55286 69.9988 190.6725 0003735 267.9603 92.1128 14.98329695 07
| Epoch (UTC): | 25 May 2026 13:41:16 |
| Eccentricity: | 0.0003735 |
| inclination: | 69.9988° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.6725° |
| argument of perigee: | 267.9603° |
| revolutions per day: | 14.98329695 |
| mean anomaly at epoch: | 92.1128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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