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 20580U 90037B 25138.60001958 .00007618 00000-0 28808-3 0 9993
2 20580 28.4680 245.4244 0002898 116.3875 243.7017 15.25020924728166
| Epoch (UTC): | 18 May 2025 14:24:01 |
| Eccentricity: | 0.0002898 |
| inclination: | 28.4680° |
| perigee height: | 489 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 245.4244° |
| argument of perigee: | 116.3875° |
| revolutions per day: | 15.25020924 |
| mean anomaly at epoch: | 243.7017° |
| orbit number at epoch: | 72816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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