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 37391U 11014B 25161.96268545 0.00000050 00000-0 67890-4 0 02
2 37391 63.4290 149.0736 0311604 356.6402 3.3598 13.40972580 07
| Epoch (UTC): | 10 June 2025 23:06:16 |
| Eccentricity: | 0.0311604 |
| inclination: | 63.4290° |
| perigee height: | 872 km |
| apogee height: | 1339 km |
| right ascension of ascending node: | 149.0736° |
| argument of perigee: | 356.6402° |
| revolutions per day: | 13.40972580 |
| mean anomaly at epoch: | 3.3598° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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