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 65687U 26145.58335647 +.00000000 +00000-0 +64289-3 0 00006
2 65687 53.1601 348.2867 0001271 93.7355 115.6437 15.31701707 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 348.2867° |
| argument of perigee: | 93.7355° |
| revolutions per day: | 15.31701707 |
| mean anomaly at epoch: | 115.6437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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