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 53497U 26145.30564786 +.00000000 +00000-0 -14629-3 0 00004
2 53497 97.4474 265.1986 0001455 169.0237 191.1022 15.05654418 00
| Epoch (UTC): | 25 May 2026 07:20:07 |
| Eccentricity: | 0.0001455 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 265.1986° |
| argument of perigee: | 169.0237° |
| revolutions per day: | 15.05654418 |
| mean anomaly at epoch: | 191.1022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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