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 60243U 26145.37770005 +.00000000 +00000-0 +52454-3 0 00008
2 60243 61.9868 288.8853 0044515 123.6615 236.8738 15.11269169 08
| Epoch (UTC): | 25 May 2026 09:03:53 |
| Eccentricity: | 0.0044515 |
| inclination: | 61.9868° |
| perigee height: | 502 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 288.8853° |
| argument of perigee: | 123.6615° |
| revolutions per day: | 15.11269169 |
| mean anomaly at epoch: | 236.8738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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