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 26384U 00033A 25140.51165108 .00000817 00000-0 14232-3 0 9999
2 26384 97.7980 126.4854 0013567 165.0593 195.1017 14.70466195330469
| Epoch (UTC): | 20 May 2025 12:16:46 |
| Eccentricity: | 0.0013567 |
| inclination: | 97.7980° |
| perigee height: | 650 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 126.4854° |
| argument of perigee: | 165.0593° |
| revolutions per day: | 14.70466195 |
| mean anomaly at epoch: | 195.1017° |
| orbit number at epoch: | 33046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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