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 55812U 26145.41323927 +.00000000 +00000-0 +25635-3 0 00007
2 55812 87.9150 309.5137 0001636 86.5409 273.5911 13.19726501 02
| Epoch (UTC): | 25 May 2026 09:55:03 |
| Eccentricity: | 0.0001636 |
| inclination: | 87.9150° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5137° |
| argument of perigee: | 86.5409° |
| revolutions per day: | 13.19726501 |
| mean anomaly at epoch: | 273.5911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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