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 60249U 26145.65388991 +.00000000 +00000-0 +21646-3 0 00003
2 60249 97.4000 224.2749 0004307 136.2035 223.9544 15.23377817 00
| Epoch (UTC): | 25 May 2026 15:41:36 |
| Eccentricity: | 0.0004307 |
| inclination: | 97.4000° |
| perigee height: | 493 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 224.2749° |
| argument of perigee: | 136.2035° |
| revolutions per day: | 15.23377817 |
| mean anomaly at epoch: | 223.9544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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