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 49299U 26145.38476544 +.00000000 +00000-0 +23880-4 0 00000
2 49299 87.9173 278.9885 0001957 101.5506 258.5847 13.20769395 01
| Epoch (UTC): | 25 May 2026 09:14:03 |
| Eccentricity: | 0.0001957 |
| inclination: | 87.9173° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9885° |
| argument of perigee: | 101.5506° |
| revolutions per day: | 13.20769395 |
| mean anomaly at epoch: | 258.5847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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