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 data is extracted from the following two-line orbital elements,
1 21949U 92023A 25188.93671991 .00000127 00000-0 39566-4 0 9993
2 21949 85.0074 272.6070 0002788 93.1933 266.9578 14.32250838 59753
| Epoch (UTC): | 07 July 2025 22:28:52 |
| Eccentricity: | 0.0002788 |
| inclination: | 85.0074° |
| perigee height: | 782 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 272.6070° |
| argument of perigee: | 93.1933° |
| revolutions per day: | 14.32250838 |
| mean anomaly at epoch: | 266.9578° |
| orbit number at epoch: | 5975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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