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 55172U 26145.39160275 +.00000000 +00000-0 -13966-2 0 00002
2 55172 87.8908 25.6154 0000920 89.5999 270.5234 13.11418188 04
| Epoch (UTC): | 25 May 2026 09:23:54 |
| Eccentricity: | 0.0000920 |
| inclination: | 87.8908° |
| perigee height: | 1217 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 25.6154° |
| argument of perigee: | 89.5999° |
| revolutions per day: | 13.11418188 |
| mean anomaly at epoch: | 270.5234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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