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 53408U 26145.35306522 +.00000000 +00000-0 +80722-5 0 00001
2 53408 53.2122 129.9708 0000987 93.5758 266.5347 15.08842629 02
| Epoch (UTC): | 25 May 2026 08:28:24 |
| Eccentricity: | 0.0000987 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 129.9708° |
| argument of perigee: | 93.5758° |
| revolutions per day: | 15.08842629 |
| mean anomaly at epoch: | 266.5347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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