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 49312U 26145.42855894 +.00000000 +00000-0 +45611-4 0 00006
2 49312 87.9181 278.9677 0002092 94.3221 265.8151 13.20771867 05
| Epoch (UTC): | 25 May 2026 10:17:07 |
| Eccentricity: | 0.0002092 |
| inclination: | 87.9181° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9677° |
| argument of perigee: | 94.3221° |
| revolutions per day: | 13.20771867 |
| mean anomaly at epoch: | 265.8151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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