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 60496U 26145.51139046 +.00000000 +00000-0 +16598-3 0 00007
2 60496 97.3755 223.6316 0002651 37.5443 322.5981 15.25859870 06
| Epoch (UTC): | 25 May 2026 12:16:24 |
| Eccentricity: | 0.0002651 |
| inclination: | 97.3755° |
| perigee height: | 486 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 223.6316° |
| argument of perigee: | 37.5443° |
| revolutions per day: | 15.25859870 |
| mean anomaly at epoch: | 322.5981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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