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 00020U 59007A 25136.75652080 .00000939 00000-0 38586-3 0 9997
2 00020 33.3413 252.9564 1643083 90.1104 288.6953 11.60643752438511
| Epoch (UTC): | 16 May 2025 18:09:23 |
| Eccentricity: | 0.1643083 |
| inclination: | 33.3413° |
| perigee height: | 508 km |
| apogee height: | 3216 km |
| right ascension of ascending node: | 252.9564° |
| argument of perigee: | 90.1104° |
| revolutions per day: | 11.60643752 |
| mean anomaly at epoch: | 288.6953° |
| orbit number at epoch: | 43851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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