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 00059U 60013B 23032.20827969 .00000146 00000-0 81109-4 0 9991
2 00059 28.2498 333.1922 0189147 53.4992 308.2819 13.53016847 76185
| Epoch (UTC): | 01 February 2023 04:59:55 |
| Eccentricity: | 0.0189147 |
| inclination: | 28.2498° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 333.1922° |
| argument of perigee: | 53.4992° |
| revolutions per day: | 13.53016847 |
| mean anomaly at epoch: | 308.2819° |
| orbit number at epoch: | 7618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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