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 60533U 26145.50779912 +.00000000 +00000-0 +70934-3 0 00004
2 60533 97.6735 227.8736 0002020 111.7698 248.3747 15.11226400 05
| Epoch (UTC): | 25 May 2026 12:11:13 |
| Eccentricity: | 0.0002020 |
| inclination: | 97.6735° |
| perigee height: | 531 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 227.8736° |
| argument of perigee: | 111.7698° |
| revolutions per day: | 15.11226400 |
| mean anomaly at epoch: | 248.3747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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