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 60481U 26145.14846969 +.00000000 +00000-0 +58673-3 0 00009
2 60481 97.3758 228.0392 0002127 17.4464 342.6854 15.39245299 05
| Epoch (UTC): | 25 May 2026 03:33:47 |
| Eccentricity: | 0.0002127 |
| inclination: | 97.3758° |
| perigee height: | 447 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 228.0392° |
| argument of perigee: | 17.4464° |
| revolutions per day: | 15.39245299 |
| mean anomaly at epoch: | 342.6854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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