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 36105U 09066B 21056.19057772 0.00000512 00000-0 26951-4 0 06
2 36105 97.2650 52.7164 0021713 308.6811 51.5040 15.15471639 09
| Epoch (UTC): | 25 February 2021 04:34:25 |
| Eccentricity: | 0.0021713 |
| inclination: | 97.2650° |
| perigee height: | 504 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 52.7164° |
| argument of perigee: | 308.6811° |
| revolutions per day: | 15.15471639 |
| mean anomaly at epoch: | 51.5040° |
| 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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