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 60538U 26144.66734139 +.00000000 +00000-0 +28627-3 0 00009
2 60538 97.6753 223.7093 0007271 96.8268 263.3785 15.02990587 03
| Epoch (UTC): | 24 May 2026 16:00:58 |
| Eccentricity: | 0.0007271 |
| inclination: | 97.6753° |
| perigee height: | 553 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 223.7093° |
| argument of perigee: | 96.8268° |
| revolutions per day: | 15.02990587 |
| mean anomaly at epoch: | 263.3785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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