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 60489U 26145.14552476 +.00000000 +00000-0 +37098-3 0 00002
2 60489 97.3693 227.0892 0003088 16.6555 343.4790 15.37368419 00
| Epoch (UTC): | 25 May 2026 03:29:33 |
| Eccentricity: | 0.0003088 |
| inclination: | 97.3693° |
| perigee height: | 452 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 227.0892° |
| argument of perigee: | 16.6555° |
| revolutions per day: | 15.37368419 |
| mean anomaly at epoch: | 343.4790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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