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 59878U 26145.43783094 +.00000000 +00000-0 +17275-2 0 00000
2 59878 42.9972 203.7012 0012766 44.1044 316.0828 15.40633762 01
| Epoch (UTC): | 25 May 2026 10:30:28 |
| Eccentricity: | 0.0012766 |
| inclination: | 42.9972° |
| perigee height: | 436 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 203.7012° |
| argument of perigee: | 44.1044° |
| revolutions per day: | 15.40633762 |
| mean anomaly at epoch: | 316.0828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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