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 55828U 26145.37130620 +.00000000 +00000-0 +11101-3 0 00008
2 55828 87.9172 278.9911 0002443 97.7397 262.4013 13.20770644 08
| Epoch (UTC): | 25 May 2026 08:54:40 |
| Eccentricity: | 0.0002443 |
| inclination: | 87.9172° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9911° |
| argument of perigee: | 97.7397° |
| revolutions per day: | 13.20770644 |
| mean anomaly at epoch: | 262.4013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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