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 29092U 06015A 23152.07401990 .00000859 00000-0 10916-3 0 9999
2 29092 97.8389 179.5761 0001537 92.1154 268.0237 14.84136621924731
| Epoch (UTC): | 01 June 2023 01:46:35 |
| Eccentricity: | 0.0001537 |
| inclination: | 97.8389° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 179.5761° |
| argument of perigee: | 92.1154° |
| revolutions per day: | 14.84136621 |
| mean anomaly at epoch: | 268.0237° |
| orbit number at epoch: | 92473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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