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 00202U 61031A 23088.82850842 .00000095 00000-0 86706-4 0 9998
2 00202 32.4370 128.6322 0101310 287.8053 71.1537 13.63601835 60464
| Epoch (UTC): | 29 March 2023 19:53:03 |
| Eccentricity: | 0.0101310 |
| inclination: | 32.4370° |
| perigee height: | 947 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 128.6322° |
| argument of perigee: | 287.8053° |
| revolutions per day: | 13.63601835 |
| mean anomaly at epoch: | 71.1537° |
| orbit number at epoch: | 6046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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