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 53683U 26145.64350166 +.00000000 +00000-0 -85664-4 0 00001
2 53683 97.4465 25.6195 0002822 84.3581 275.7968 15.05657954 04
| Epoch (UTC): | 25 May 2026 15:26:38 |
| Eccentricity: | 0.0002822 |
| inclination: | 97.4465° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.6195° |
| argument of perigee: | 84.3581° |
| revolutions per day: | 15.05657954 |
| mean anomaly at epoch: | 275.7968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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