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 21090U 91007B 25198.48100372 -.00000026 00000-0 -42589-4 0 9991
2 21090 82.9197 199.6682 0021917 63.8488 296.4920 13.76629422729853
Epoch (UTC): | 17 July 2025 11:32:38 |
Eccentricity: | 0.0021917 |
inclination: | 82.9197° |
perigee height: | 960 km |
apogee height: | 992 km |
right ascension of ascending node: | 199.6682° |
argument of perigee: | 63.8488° |
revolutions per day: | 13.76629422 |
mean anomaly at epoch: | 296.4920° |
orbit number at epoch: | 72985 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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