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 00011U 59001A 25173.58321075 .00001108 00000-0 57192-3 0 9993
2 00011 32.8704 5.5398 1448620 171.3636 191.4996 11.89887639492611
| Epoch (UTC): | 22 June 2025 13:59:49 |
| Eccentricity: | 0.1448620 |
| inclination: | 32.8704° |
| perigee height: | 552 km |
| apogee height: | 2900 km |
| right ascension of ascending node: | 5.5398° |
| argument of perigee: | 171.3636° |
| revolutions per day: | 11.89887639 |
| mean anomaly at epoch: | 191.4996° |
| orbit number at epoch: | 49261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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