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 60327U 26145.61377948 +.00000000 +00000-0 +00000-0 0 00004
2 60327 0.0429 355.0868 0008012 10.2280 252.0322 1.00270290 01
| Epoch (UTC): | 25 May 2026 14:43:50 |
| Eccentricity: | 0.0008012 |
| inclination: | 0.0429° |
| perigee height: | 35753 km |
| apogee height: | 35821 km |
| right ascension of ascending node: | 355.0868° |
| argument of perigee: | 10.2280° |
| revolutions per day: | 1.00270290 |
| mean anomaly at epoch: | 252.0322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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