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 60474U 26145.49505700 +.00000000 +00000-0 +39134-3 0 00005
2 60474 97.3768 228.7149 0001139 36.3307 323.8015 15.38938022 05
| Epoch (UTC): | 25 May 2026 11:52:52 |
| Eccentricity: | 0.0001139 |
| inclination: | 97.3768° |
| perigee height: | 448 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 228.7149° |
| argument of perigee: | 36.3307° |
| revolutions per day: | 15.38938022 |
| mean anomaly at epoch: | 323.8015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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