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 60548U 26145.16860354 +.00000000 +00000-0 +28314-3 0 00008
2 60548 97.7197 224.4460 0000430 130.0039 230.1223 15.00902357 05
| Epoch (UTC): | 25 May 2026 04:02:47 |
| Eccentricity: | 0.0000430 |
| inclination: | 97.7197° |
| perigee height: | 564 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 224.4460° |
| argument of perigee: | 130.0039° |
| revolutions per day: | 15.00902357 |
| mean anomaly at epoch: | 230.1223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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