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 60360U 26145.18699530 +.00000000 +00000-0 +38349-4 0 00008
2 60360 53.1595 314.0014 0001254 95.1909 264.9236 15.31702508 07
| Epoch (UTC): | 25 May 2026 04:29:16 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 314.0014° |
| argument of perigee: | 95.1909° |
| revolutions per day: | 15.31702508 |
| mean anomaly at epoch: | 264.9236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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