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 55155U 26145.31998125 +.00000000 +00000-0 +95570-4 0 00000
2 55155 87.9151 10.4122 0001671 77.6075 282.5243 13.17651644 05
| Epoch (UTC): | 25 May 2026 07:40:46 |
| Eccentricity: | 0.0001671 |
| inclination: | 87.9151° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4122° |
| argument of perigee: | 77.6075° |
| revolutions per day: | 13.17651644 |
| mean anomaly at epoch: | 282.5243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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