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 60203U 26145.09284634 +.00000000 +00000-0 +56866-3 0 00002
2 60203 97.2316 2.9666 0007673 293.6203 66.4250 15.63465099 09
| Epoch (UTC): | 25 May 2026 02:13:41 |
| Eccentricity: | 0.0007673 |
| inclination: | 97.2316° |
| perigee height: | 372 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 2.9666° |
| argument of perigee: | 293.6203° |
| revolutions per day: | 15.63465099 |
| mean anomaly at epoch: | 66.4250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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