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 59269U 26145.48178999 +.00000000 +00000-0 +27820-4 0 00000
2 59269 53.1595 184.4515 0000991 91.3096 268.8018 15.30186372 05
| Epoch (UTC): | 25 May 2026 11:33:46 |
| Eccentricity: | 0.0000991 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.4515° |
| argument of perigee: | 91.3096° |
| revolutions per day: | 15.30186372 |
| mean anomaly at epoch: | 268.8018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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