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 49199U 26145.43922662 +.00000000 +00000-0 -53672-3 0 00004
2 49199 87.8941 324.7677 0001833 90.2433 269.8906 13.13467996 02
| Epoch (UTC): | 25 May 2026 10:32:29 |
| Eccentricity: | 0.0001833 |
| inclination: | 87.8941° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7677° |
| argument of perigee: | 90.2433° |
| revolutions per day: | 13.13467996 |
| mean anomaly at epoch: | 269.8906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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