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 53679U 26145.61438325 +.00000000 +00000-0 -98060-4 0 00001
2 53679 97.4476 26.7373 0002272 93.4504 266.6983 15.05660571 01
| Epoch (UTC): | 25 May 2026 14:44:42 |
| Eccentricity: | 0.0002272 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.7373° |
| argument of perigee: | 93.4504° |
| revolutions per day: | 15.05660571 |
| mean anomaly at epoch: | 266.6983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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