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 59376U 26145.58043369 +.00000000 +00000-0 +26180-4 0 00000
2 59376 53.1606 258.5204 0001288 87.7844 272.3305 15.30193546 05
| Epoch (UTC): | 25 May 2026 13:55:49 |
| Eccentricity: | 0.0001288 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 258.5204° |
| argument of perigee: | 87.7844° |
| revolutions per day: | 15.30193546 |
| mean anomaly at epoch: | 272.3305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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