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 55839U 26145.58917075 +.00000000 +00000-0 +26514-3 0 00004
2 55839 99.0136 154.0965 0001532 72.5996 287.5337 14.01351645 04
| Epoch (UTC): | 25 May 2026 14:08:24 |
| Eccentricity: | 0.0001532 |
| inclination: | 99.0136° |
| perigee height: | 888 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 154.0965° |
| argument of perigee: | 72.5996° |
| revolutions per day: | 14.01351645 |
| mean anomaly at epoch: | 287.5337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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