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 60748U 26145.63301213 +.00000000 +00000-0 +53905-3 0 00000
2 60748 97.6757 282.8865 0000642 263.7244 96.3921 15.27132344 09
| Epoch (UTC): | 25 May 2026 15:11:32 |
| Eccentricity: | 0.0000642 |
| inclination: | 97.6757° |
| perigee height: | 484 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 282.8865° |
| argument of perigee: | 263.7244° |
| revolutions per day: | 15.27132344 |
| mean anomaly at epoch: | 96.3921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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