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 23730U 26150.29696110 +.00000000 +00000-0 +00000-0 0 00006
2 23730 14.0888 16.1992 0014348 306.9188 251.8632 0.97937963 09
| Epoch (UTC): | 30 May 2026 07:07:37 |
| Eccentricity: | 0.0014348 |
| inclination: | 14.0888° |
| perigee height: | 36392 km |
| apogee height: | 36515 km |
| right ascension of ascending node: | 16.1992° |
| argument of perigee: | 306.9188° |
| revolutions per day: | 0.97937963 |
| mean anomaly at epoch: | 251.8632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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