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 04256U 69082B 22225.91376848 .00000079 00000-0 92282-4 0 9994
2 04256 70.0096 97.7199 0016974 102.9728 257.3276 13.98470190694226
| Epoch (UTC): | 13 August 2022 21:55:49 |
| Eccentricity: | 0.0016974 |
| inclination: | 70.0096° |
| perigee height: | 887 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 97.7199° |
| argument of perigee: | 102.9728° |
| revolutions per day: | 13.98470190 |
| mean anomaly at epoch: | 257.3276° |
| orbit number at epoch: | 69422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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