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 49309U 26145.42452610 +.00000000 +00000-0 +46294-4 0 00009
2 49309 87.8954 294.2376 0001921 92.8989 267.2360 13.14504227 04
| Epoch (UTC): | 25 May 2026 10:11:19 |
| Eccentricity: | 0.0001921 |
| inclination: | 87.8954° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2376° |
| argument of perigee: | 92.8989° |
| revolutions per day: | 13.14504227 |
| mean anomaly at epoch: | 267.2360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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