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 60749U 26145.64969720 +.00000000 +00000-0 +61028-3 0 00000
2 60749 97.6686 282.3824 0001947 40.2111 319.9271 15.26319402 04
| Epoch (UTC): | 25 May 2026 15:35:33 |
| Eccentricity: | 0.0001947 |
| inclination: | 97.6686° |
| perigee height: | 485 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 282.3824° |
| argument of perigee: | 40.2111° |
| revolutions per day: | 15.26319402 |
| mean anomaly at epoch: | 319.9271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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