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 53650U 26145.62410591 +.00000000 +00000-0 -42636-4 0 00004
2 53650 97.4504 25.5932 0002832 69.9871 290.1661 15.05659871 03
| Epoch (UTC): | 25 May 2026 14:58:42 |
| Eccentricity: | 0.0002832 |
| inclination: | 97.4504° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.5932° |
| argument of perigee: | 69.9871° |
| revolutions per day: | 15.05659871 |
| mean anomaly at epoch: | 290.1661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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