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 55162U 26145.12372244 +.00000000 +00000-0 +13754-2 0 00007
2 55162 87.8917 25.6531 0002020 85.1772 274.9587 13.11415084 07
| Epoch (UTC): | 25 May 2026 02:58:09 |
| Eccentricity: | 0.0002020 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6531° |
| argument of perigee: | 85.1772° |
| revolutions per day: | 13.11415084 |
| mean anomaly at epoch: | 274.9587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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