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 54139U 26145.41797782 +.00000000 +00000-0 +13312-3 0 00001
2 54139 87.9161 309.4919 0002065 93.9276 266.2093 13.19725906 01
| Epoch (UTC): | 25 May 2026 10:01:53 |
| Eccentricity: | 0.0002065 |
| inclination: | 87.9161° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4919° |
| argument of perigee: | 93.9276° |
| revolutions per day: | 13.19725906 |
| mean anomaly at epoch: | 266.2093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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