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 49314U 26145.35954029 +.00000000 +00000-0 +10530-3 0 00001
2 49314 87.9152 309.5206 0001942 92.4846 267.6508 13.19725770 05
| Epoch (UTC): | 25 May 2026 08:37:44 |
| Eccentricity: | 0.0001942 |
| inclination: | 87.9152° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5206° |
| argument of perigee: | 92.4846° |
| revolutions per day: | 13.19725770 |
| mean anomaly at epoch: | 267.6508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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