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 22179.31500584 .00000504 00000-0 10420-3 0 9990
2 28895 98.1081 310.5265 0017988 106.4933 253.8248 14.64363177889001
| Epoch (UTC): | 28 June 2022 07:33:36 |
| Eccentricity: | 0.0017988 |
| inclination: | 98.1081° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 310.5265° |
| argument of perigee: | 106.4933° |
| revolutions per day: | 14.64363177 |
| mean anomaly at epoch: | 253.8248° |
| orbit number at epoch: | 88900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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