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 49085U 26145.28652235 +.00000000 +00000-0 -23466-3 0 00005
2 49085 87.8962 355.2195 0001835 97.1047 263.0291 13.12441025 09
| Epoch (UTC): | 25 May 2026 06:52:35 |
| Eccentricity: | 0.0001835 |
| inclination: | 87.8962° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2195° |
| argument of perigee: | 97.1047° |
| revolutions per day: | 13.12441025 |
| mean anomaly at epoch: | 263.0291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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