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 85U 61004C 23029.38420016 .00009019 00000-0 17131-2 0 9998
2 85 38.7624 159.6812 0359474 61.7479 301.9069 14.30062288 67367
| Epoch (UTC): | 29 January 2023 09:13:14 |
| Eccentricity: | 0.0359474 |
| inclination: | 38.7624° |
| perigee height: | 534 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 159.6812° |
| argument of perigee: | 61.7479° |
| revolutions per day: | 14.30062288 |
| mean anomaly at epoch: | 301.9069° |
| orbit number at epoch: | 6736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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