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 28888U 05042A 23086.83755332 0.00015681 00000-0 26833-3 0 09
2 28888 97.1271 126.5345 0030159 359.4634 0.4298 15.50724722 09
| Epoch (UTC): | 27 March 2023 20:06:04 |
| Eccentricity: | 0.0030159 |
| inclination: | 97.1271° |
| perigee height: | 394 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 126.5345° |
| argument of perigee: | 359.4634° |
| revolutions per day: | 15.50724722 |
| mean anomaly at epoch: | 0.4298° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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