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 22274.08436533 .00001421 00000-0 27658-3 0 9992
2 28895 98.1209 43.9268 0016939 164.8680 195.3033 14.64507046903100
| Epoch (UTC): | 01 October 2022 02:01:29 |
| Eccentricity: | 0.0016939 |
| inclination: | 98.1209° |
| perigee height: | 667 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 43.9268° |
| argument of perigee: | 164.8680° |
| revolutions per day: | 14.64507046 |
| mean anomaly at epoch: | 195.3033° |
| orbit number at epoch: | 90310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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