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 56846U 26145.58448043 +.00000000 +00000-0 +38481-3 0 00003
2 56846 97.3709 216.0926 0001138 90.8673 269.2694 15.22886818 05
| Epoch (UTC): | 25 May 2026 14:01:39 |
| Eccentricity: | 0.0001138 |
| inclination: | 97.3709° |
| perigee height: | 496 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 216.0926° |
| argument of perigee: | 90.8673° |
| revolutions per day: | 15.22886818 |
| mean anomaly at epoch: | 269.2694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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