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 55830U 26145.47009255 +.00000000 +00000-0 +32058-3 0 00005
2 55830 87.9150 309.5049 0001784 87.8250 272.3086 13.19727396 09
| Epoch (UTC): | 25 May 2026 11:16:55 |
| Eccentricity: | 0.0001784 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5049° |
| argument of perigee: | 87.8250° |
| revolutions per day: | 13.19727396 |
| mean anomaly at epoch: | 272.3086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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