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 60948U 26145.63485655 +.00000000 +00000-0 +30412-3 0 00003
2 60948 34.9928 339.7868 0002443 20.0288 340.0522 15.23015803 05
| Epoch (UTC): | 25 May 2026 15:14:11 |
| Eccentricity: | 0.0002443 |
| inclination: | 34.9928° |
| perigee height: | 495 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 339.7868° |
| argument of perigee: | 20.0288° |
| revolutions per day: | 15.23015803 |
| mean anomaly at epoch: | 340.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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