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 60023U 26145.24068289 +.00000000 +00000-0 +31298-4 0 00008
2 60023 53.1605 80.0683 0001246 86.0444 274.0699 15.30198693 09
| Epoch (UTC): | 25 May 2026 05:46:35 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.0683° |
| argument of perigee: | 86.0444° |
| revolutions per day: | 15.30198693 |
| mean anomaly at epoch: | 274.0699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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