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 56880U 26145.01404551 +.00000000 +00000-0 +97127-5 0 00009
2 56880 43.0042 14.1274 0000918 257.0560 103.0189 15.26741625 05
| Epoch (UTC): | 25 May 2026 00:20:13 |
| Eccentricity: | 0.0000918 |
| inclination: | 43.0042° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 14.1274° |
| argument of perigee: | 257.0560° |
| revolutions per day: | 15.26741625 |
| mean anomaly at epoch: | 103.0189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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