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 55803U 26145.43851874 +.00000000 +00000-0 -23359-4 0 00009
2 55803 87.9150 309.5114 0001003 68.9652 291.1588 13.19726178 05
| Epoch (UTC): | 25 May 2026 10:31:28 |
| Eccentricity: | 0.0001003 |
| inclination: | 87.9150° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5114° |
| argument of perigee: | 68.9652° |
| revolutions per day: | 13.19726178 |
| mean anomaly at epoch: | 291.1588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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