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 61049U 26145.03402810 +.00000000 +00000-0 +93315-3 0 00003
2 61049 52.9774 55.4014 0010471 73.5766 286.6378 15.20829544 02
| Epoch (UTC): | 25 May 2026 00:49:00 |
| Eccentricity: | 0.0010471 |
| inclination: | 52.9774° |
| perigee height: | 496 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 55.4014° |
| argument of perigee: | 73.5766° |
| revolutions per day: | 15.20829544 |
| mean anomaly at epoch: | 286.6378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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