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 28654U 05018A 22176.13843767 .00000130 00000-0 94010-4 0 9998
2 28654 98.9488 246.5683 0013309 312.6201 47.3848 14.12745681881154
| Epoch (UTC): | 25 June 2022 03:19:21 |
| Eccentricity: | 0.0013309 |
| inclination: | 98.9488° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 246.5683° |
| argument of perigee: | 312.6201° |
| revolutions per day: | 14.12745681 |
| mean anomaly at epoch: | 47.3848° |
| orbit number at epoch: | 88115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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