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 35934U 09051D 23088.85809267 .00001487 00000-0 34331-3 0 9992
2 35934 98.5434 314.8712 0005240 274.0081 86.0517 14.56744612717538
Epoch (UTC): | 29 March 2023 20:35:39 |
Eccentricity: | 0.0005240 |
inclination: | 98.5434° |
perigee height: | 700 km |
apogee height: | 707 km |
right ascension of ascending node: | 314.8712° |
argument of perigee: | 274.0081° |
revolutions per day: | 14.56744612 |
mean anomaly at epoch: | 86.0517° |
orbit number at epoch: | 71753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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