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 23153.55169598 .00007343 00000-0 38354-3 0 9992
2 26960 97.7831 184.3135 0045386 321.0290 38.7673 15.15317797182234
| Epoch (UTC): | 02 June 2023 13:14:26 |
| Eccentricity: | 0.0045386 |
| inclination: | 97.7831° |
| perigee height: | 489 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 184.3135° |
| argument of perigee: | 321.0290° |
| revolutions per day: | 15.15317797 |
| mean anomaly at epoch: | 38.7673° |
| orbit number at epoch: | 18223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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