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 12988U 81117B 22228.39594800 .00000271 00000-0 28772-4 0 9990
2 12988 82.5234 103.8171 0019542 94.6312 265.7136 14.84986244178658
| Epoch (UTC): | 16 August 2022 09:30:09 |
| Eccentricity: | 0.0019542 |
| inclination: | 82.5234° |
| perigee height: | 600 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 103.8171° |
| argument of perigee: | 94.6312° |
| revolutions per day: | 14.84986244 |
| mean anomaly at epoch: | 265.7136° |
| orbit number at epoch: | 17865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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