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 27844U 03031E 22179.89205261 .00000138 00000-0 81454-4 0 9994
2 27844 98.6776 187.4053 0011097 71.5333 288.7051 14.22459719985498
| Epoch (UTC): | 28 June 2022 21:24:33 |
| Eccentricity: | 0.0011097 |
| inclination: | 98.6776° |
| perigee height: | 809 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 187.4053° |
| argument of perigee: | 71.5333° |
| revolutions per day: | 14.22459719 |
| mean anomaly at epoch: | 288.7051° |
| orbit number at epoch: | 98549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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