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 30088U 99025QR 23033.52215383 .00000757 00000-0 23612-3 0 9990
2 30088 98.3074 46.2095 0215920 119.2656 30.6572 14.31021671837138
| Epoch (UTC): | 02 February 2023 12:31:54 |
| Eccentricity: | 0.0215920 |
| inclination: | 98.3074° |
| perigee height: | 633 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 46.2095° |
| argument of perigee: | 119.2656° |
| revolutions per day: | 14.31021671 |
| mean anomaly at epoch: | 30.6572° |
| orbit number at epoch: | 83713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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