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 25338U 98030A 23087.20260464 .00000327 00000-0 15449-3 0 9993
2 25338 98.6157 117.6113 0010397 184.0284 176.0814 14.26277679293716
| Epoch (UTC): | 28 March 2023 04:51:45 |
| Eccentricity: | 0.0010397 |
| inclination: | 98.6157° |
| perigee height: | 797 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 117.6113° |
| argument of perigee: | 184.0284° |
| revolutions per day: | 14.26277679 |
| mean anomaly at epoch: | 176.0814° |
| orbit number at epoch: | 29371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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