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 31988U 99025CPR 24275.50753934 .00014627 00000-0 74410-2 0 9998
2 31988 98.1502 14.5473 0067222 127.0215 233.7136 14.14706244579556
| Epoch (UTC): | 01 October 2024 12:10:51 |
| Eccentricity: | 0.0067222 |
| inclination: | 98.1502° |
| perigee height: | 795 km |
| apogee height: | 892 km |
| right ascension of ascending node: | 14.5473° |
| argument of perigee: | 127.0215° |
| revolutions per day: | 14.14706244 |
| mean anomaly at epoch: | 233.7136° |
| orbit number at epoch: | 57955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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