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 53671U 26145.23088709 +.00000000 +00000-0 -11972-3 0 00004
2 53671 97.4522 25.1363 0002069 79.1496 280.9964 15.05658351 03
| Epoch (UTC): | 25 May 2026 05:32:28 |
| Eccentricity: | 0.0002069 |
| inclination: | 97.4522° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.1363° |
| argument of perigee: | 79.1496° |
| revolutions per day: | 15.05658351 |
| mean anomaly at epoch: | 280.9964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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