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 60309U 26145.13319762 +.00000000 +00000-0 +18904-5 0 00008
2 60309 53.1586 129.1473 0000902 84.8863 275.2258 15.69707421 06
| Epoch (UTC): | 25 May 2026 03:11:48 |
| Eccentricity: | 0.0000902 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 129.1473° |
| argument of perigee: | 84.8863° |
| revolutions per day: | 15.69707421 |
| mean anomaly at epoch: | 275.2258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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