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 59845U 26145.49260044 +.00000000 +00000-0 -33941-4 0 00006
2 59845 43.0000 193.6180 0001222 272.2458 87.8253 15.27573402 04
| Epoch (UTC): | 25 May 2026 11:49:20 |
| Eccentricity: | 0.0001222 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.6180° |
| argument of perigee: | 272.2458° |
| revolutions per day: | 15.27573402 |
| mean anomaly at epoch: | 87.8253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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