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 60235U 26129.87036027 +.00000000 +00000-0 +13688-3 0 00001
2 60235 61.9955 4.5034 0055042 126.7879 233.8281 15.00958115 07
| Epoch (UTC): | 09 May 2026 20:53:19 |
| Eccentricity: | 0.0055042 |
| inclination: | 61.9955° |
| perigee height: | 526 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 4.5034° |
| argument of perigee: | 126.7879° |
| revolutions per day: | 15.00958115 |
| mean anomaly at epoch: | 233.8281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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