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 28375U 04025K 20333.60171593 +.00000050 +00000-0 +27896-4 0 9990
2 28375 098.4449 262.3439 0083643 086.7989 274.2766 14.41980419863399
| Epoch (UTC): | 28 November 2020 14:26:28 |
| Eccentricity: | 0.0083643 |
| inclination: | 98.4449° |
| perigee height: | 692 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 262.3439° |
| argument of perigee: | 86.7989° |
| revolutions per day: | 14.41980419 |
| mean anomaly at epoch: | 274.2766° |
| orbit number at epoch: | 86339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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