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 60084U 26145.56518012 +.00000000 +00000-0 +10782-3 0 00008
2 60084 97.8926 169.4457 0003504 192.0850 168.0278 14.80580030 05
| Epoch (UTC): | 25 May 2026 13:33:51 |
| Eccentricity: | 0.0003504 |
| inclination: | 97.8926° |
| perigee height: | 625 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 169.4457° |
| argument of perigee: | 192.0850° |
| revolutions per day: | 14.80580030 |
| mean anomaly at epoch: | 168.0278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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