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 39152U 13018C 25138.22882263 .00004233 00000-0 41341-3 0 9993
2 39152 97.8069 226.4152 0012155 340.4113 19.6638 14.92877576652106
| Epoch (UTC): | 18 May 2025 05:29:30 |
| Eccentricity: | 0.0012155 |
| inclination: | 97.8069° |
| perigee height: | 580 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 226.4152° |
| argument of perigee: | 340.4113° |
| revolutions per day: | 14.92877576 |
| mean anomaly at epoch: | 19.6638° |
| orbit number at epoch: | 65210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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