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 59894U 26145.42658781 +.00000000 +00000-0 +39348-5 0 00009
2 59894 43.0020 45.0331 0001004 272.6088 87.4648 15.27573032 02
| Epoch (UTC): | 25 May 2026 10:14:17 |
| Eccentricity: | 0.0001004 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 45.0331° |
| argument of perigee: | 272.6088° |
| revolutions per day: | 15.27573032 |
| mean anomaly at epoch: | 87.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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