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 59435U 26145.64795981 +.00000000 +00000-0 +42752-4 0 00000
2 59435 53.1621 284.0987 0001234 90.6884 269.4259 15.30191951 01
| Epoch (UTC): | 25 May 2026 15:33:03 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 284.0987° |
| argument of perigee: | 90.6884° |
| revolutions per day: | 15.30191951 |
| mean anomaly at epoch: | 269.4259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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