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 00005U 58002B 25140.53135029 .00000085 00000-0 10276-3 0 9992
2 00005 34.2455 86.2388 1840993 168.1250 196.9621 10.85923198400590
| Epoch (UTC): | 20 May 2025 12:45:08 |
| Eccentricity: | 0.1840993 |
| inclination: | 34.2455° |
| perigee height: | 650 km |
| apogee height: | 3821 km |
| right ascension of ascending node: | 86.2388° |
| argument of perigee: | 168.1250° |
| revolutions per day: | 10.85923198 |
| mean anomaly at epoch: | 196.9621° |
| orbit number at epoch: | 40059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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