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 28895U 05043F 23091.32920243 .00003439 00000-0 64485-3 0 9993
2 28895 98.1395 224.0486 0015362 317.0697 42.9306 14.65327838929556
| Epoch (UTC): | 01 April 2023 07:54:03 |
| Eccentricity: | 0.0015362 |
| inclination: | 98.1395° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 224.0486° |
| argument of perigee: | 317.0697° |
| revolutions per day: | 14.65327838 |
| mean anomaly at epoch: | 42.9306° |
| orbit number at epoch: | 92955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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