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 54173U 26145.06505383 +.00000000 +00000-0 -86015-4 0 00006
2 54173 53.2141 20.8374 0001402 105.6942 254.4205 15.08847185 05
| Epoch (UTC): | 25 May 2026 01:33:40 |
| Eccentricity: | 0.0001402 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 20.8374° |
| argument of perigee: | 105.6942° |
| revolutions per day: | 15.08847185 |
| mean anomaly at epoch: | 254.4205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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