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 60488U 26145.13531941 +.00000000 +00000-0 +45657-3 0 00004
2 60488 97.3799 230.0969 0002164 33.5544 326.5841 15.43087734 09
| Epoch (UTC): | 25 May 2026 03:14:51 |
| Eccentricity: | 0.0002164 |
| inclination: | 97.3799° |
| perigee height: | 436 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 230.0969° |
| argument of perigee: | 33.5544° |
| revolutions per day: | 15.43087734 |
| mean anomaly at epoch: | 326.5841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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