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 28384U 04034A 23059.73501005 0.00000000 00000-0 00000-0 0 09
2 28384 64.2452 29.0379 7456969 264.2840 97.1540 2.00668893 00
| Epoch (UTC): | 28 February 2023 17:38:24 |
| Eccentricity: | 0.7456969 |
| inclination: | 64.2452° |
| perigee height: | 374 km |
| apogee height: | 39971 km |
| right ascension of ascending node: | 29.0379° |
| argument of perigee: | 264.2840° |
| revolutions per day: | 2.00668893 |
| mean anomaly at epoch: | 97.1540° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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