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 26930U 01043B 23088.86171564 .00000228 00000-0 11834-3 0 9999
2 26930 67.0034 347.6369 0002247 259.6881 100.3967 14.30898714122538
| Epoch (UTC): | 29 March 2023 20:40:52 |
| Eccentricity: | 0.0002247 |
| inclination: | 67.0034° |
| perigee height: | 787 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 347.6369° |
| argument of perigee: | 259.6881° |
| revolutions per day: | 14.30898714 |
| mean anomaly at epoch: | 100.3967° |
| orbit number at epoch: | 12253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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