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 57821U 26145.52874625 +.00000000 +00000-0 +13603-3 0 00009
2 57821 42.9996 160.7648 0001465 270.5718 89.4966 15.27577396 06
| Epoch (UTC): | 25 May 2026 12:41:23 |
| Eccentricity: | 0.0001465 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.7648° |
| argument of perigee: | 270.5718° |
| revolutions per day: | 15.27577396 |
| mean anomaly at epoch: | 89.4966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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