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 43134U 18004Z 23277.31342337 .00204531 00000-0 16013-2 0 9993
2 43134 97.3167 1.6139 0001248 103.1482 256.9920 15.70976128319411
| Epoch (UTC): | 04 October 2023 07:31:19 |
| Eccentricity: | 0.0001248 |
| inclination: | 97.3167° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 1.6139° |
| argument of perigee: | 103.1482° |
| revolutions per day: | 15.70976128 |
| mean anomaly at epoch: | 256.9920° |
| orbit number at epoch: | 31941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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