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 56774U 26145.52421307 +.00000000 +00000-0 +37889-3 0 00002
2 56774 69.9987 170.8273 0003668 266.3329 93.7410 14.98308604 08
| Epoch (UTC): | 25 May 2026 12:34:52 |
| Eccentricity: | 0.0003668 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.8273° |
| argument of perigee: | 266.3329° |
| revolutions per day: | 14.98308604 |
| mean anomaly at epoch: | 93.7410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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