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 59389U 26145.34451088 +.00000000 +00000-0 +24002-3 0 00009
2 59389 53.1588 259.9257 0001579 101.7675 258.3502 15.30203529 09
| Epoch (UTC): | 25 May 2026 08:16:05 |
| Eccentricity: | 0.0001579 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 259.9257° |
| argument of perigee: | 101.7675° |
| revolutions per day: | 15.30203529 |
| mean anomaly at epoch: | 258.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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