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 26960U 01049D 22148.80100424 .00004523 00000-0 27086-3 0 9993
2 26960 97.8143 166.4699 0053180 143.1368 217.3536 15.10341918126358
| Epoch (UTC): | 28 May 2022 19:13:26 |
| Eccentricity: | 0.0053180 |
| inclination: | 97.8143° |
| perigee height: | 498 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 166.4699° |
| argument of perigee: | 143.1368° |
| revolutions per day: | 15.10341918 |
| mean anomaly at epoch: | 217.3536° |
| orbit number at epoch: | 12635 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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