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 59641U 26145.50837370 +.00000000 +00000-0 +11585-3 0 00002
2 59641 43.0050 65.6942 0000758 253.2181 106.8587 15.27576153 00
| Epoch (UTC): | 25 May 2026 12:12:03 |
| Eccentricity: | 0.0000758 |
| inclination: | 43.0050° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.6942° |
| argument of perigee: | 253.2181° |
| revolutions per day: | 15.27576153 |
| mean anomaly at epoch: | 106.8587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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