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 60082U 26145.60830051 +.00000000 +00000-0 +89255-4 0 00003
2 60082 97.9887 165.9900 0000220 130.6601 229.4627 14.76222426 05
| Epoch (UTC): | 25 May 2026 14:35:57 |
| Eccentricity: | 0.0000220 |
| inclination: | 97.9887° |
| perigee height: | 641 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 165.9900° |
| argument of perigee: | 130.6601° |
| revolutions per day: | 14.76222426 |
| mean anomaly at epoch: | 229.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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