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 04157U 69082Z 23335.34124159 .00013100 00000-0 16907-2 0 9997
2 04157 70.0183 314.0618 0031204 39.8333 320.5099 14.80773590855471
| Epoch (UTC): | 01 December 2023 08:11:23 |
| Eccentricity: | 0.0031204 |
| inclination: | 70.0183° |
| perigee height: | 605 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 314.0618° |
| argument of perigee: | 39.8333° |
| revolutions per day: | 14.80773590 |
| mean anomaly at epoch: | 320.5099° |
| orbit number at epoch: | 85547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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