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 57154U 26145.60071542 +.00000000 +00000-0 +15466-4 0 00004
2 57154 43.0019 189.1733 0001214 271.2611 88.8102 15.27577176 06
| Epoch (UTC): | 25 May 2026 14:25:01 |
| Eccentricity: | 0.0001214 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.1733° |
| argument of perigee: | 271.2611° |
| revolutions per day: | 15.27577176 |
| mean anomaly at epoch: | 88.8102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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