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 60385U 26145.60309765 +.00000000 +00000-0 +16953-3 0 00006
2 60385 88.9757 274.4284 0013965 212.6899 147.3433 14.27813059 05
| Epoch (UTC): | 25 May 2026 14:28:27 |
| Eccentricity: | 0.0013965 |
| inclination: | 88.9757° |
| perigee height: | 789 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 274.4284° |
| argument of perigee: | 212.6899° |
| revolutions per day: | 14.27813059 |
| mean anomaly at epoch: | 147.3433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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