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 23276.53554814 .00000297 00000-0 14140-3 0 9997
2 25338 98.5989 303.7077 0010294 4.0360 356.0901 14.26401245320702
| Epoch (UTC): | 03 October 2023 12:51:11 |
| Eccentricity: | 0.0010294 |
| inclination: | 98.5989° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 303.7077° |
| argument of perigee: | 4.0360° |
| revolutions per day: | 14.26401245 |
| mean anomaly at epoch: | 356.0901° |
| orbit number at epoch: | 32070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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