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 29982U 99025LG 23160.72510916 .00001599 00000-0 31766-3 0 9998
2 29982 99.3875 209.0540 0141403 177.0618 299.4957 14.57756674868937
| Epoch (UTC): | 09 June 2023 17:24:09 |
| Eccentricity: | 0.0141403 |
| inclination: | 99.3875° |
| perigee height: | 600 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 209.0540° |
| argument of perigee: | 177.0618° |
| revolutions per day: | 14.57756674 |
| mean anomaly at epoch: | 299.4957° |
| orbit number at epoch: | 86893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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