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 60536U 26145.21511147 +.00000000 +00000-0 +63972-3 0 00003
2 60536 97.6878 228.0053 0002606 158.2291 201.9049 15.10698331 01
| Epoch (UTC): | 25 May 2026 05:09:45 |
| Eccentricity: | 0.0002606 |
| inclination: | 97.6878° |
| perigee height: | 532 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 228.0053° |
| argument of perigee: | 158.2291° |
| revolutions per day: | 15.10698331 |
| mean anomaly at epoch: | 201.9049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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