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 00694U 63047A 23150.85868400 .00001088 00000-0 12523-3 0 9992
2 00694 30.3573 72.0033 0575109 191.8984 166.7490 14.05252199988550
| Epoch (UTC): | 30 May 2023 20:36:30 |
| Eccentricity: | 0.0575109 |
| inclination: | 30.3573° |
| perigee height: | 458 km |
| apogee height: | 1293 km |
| right ascension of ascending node: | 72.0033° |
| argument of perigee: | 191.8984° |
| revolutions per day: | 14.05252199 |
| mean anomaly at epoch: | 166.7490° |
| orbit number at epoch: | 98855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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