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 25407U 98045B 23153.43543377 .00000120 00000-0 85134-4 0 9992
2 25407 71.0097 147.7423 0005901 140.1066 220.0492 14.15917184283941
| Epoch (UTC): | 02 June 2023 10:27:01 |
| Eccentricity: | 0.0005901 |
| inclination: | 71.0097° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 147.7423° |
| argument of perigee: | 140.1066° |
| revolutions per day: | 14.15917184 |
| mean anomaly at epoch: | 220.0492° |
| orbit number at epoch: | 28394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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