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 25119U 97084H 23088.84136654 .00003095 00000-0 10060-2 0 9990
2 25119 45.0148 280.7837 0003812 100.1089 260.0191 14.40583453324476
| Epoch (UTC): | 29 March 2023 20:11:34 |
| Eccentricity: | 0.0003812 |
| inclination: | 45.0148° |
| perigee height: | 754 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 280.7837° |
| argument of perigee: | 100.1089° |
| revolutions per day: | 14.40583453 |
| mean anomaly at epoch: | 260.0191° |
| orbit number at epoch: | 32447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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