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 28420U 04037B 23274.17297045 .00000011 00000-0 72159-5 0 9994
2 28420 82.4844 228.8111 0012660 292.1373 67.8364 12.45293704864596
| Epoch (UTC): | 01 October 2023 04:09:04 |
| Eccentricity: | 0.0012660 |
| inclination: | 82.4844° |
| perigee height: | 1474 km |
| apogee height: | 1494 km |
| right ascension of ascending node: | 228.8111° |
| argument of perigee: | 292.1373° |
| revolutions per day: | 12.45293704 |
| mean anomaly at epoch: | 67.8364° |
| orbit number at epoch: | 86459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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