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 27821U 03024B 25192.93937382 .00007304 00000-0 75803-3 0 9992
2 27821 49.4830 59.4696 4713634 193.3631 147.8253 6.13683521453808
| Epoch (UTC): | 11 July 2025 22:32:41 |
| Eccentricity: | 0.4713634 |
| inclination: | 49.4830° |
| perigee height: | 284 km |
| apogee height: | 12164 km |
| right ascension of ascending node: | 59.4696° |
| argument of perigee: | 193.3631° |
| revolutions per day: | 6.13683521 |
| mean anomaly at epoch: | 147.8253° |
| orbit number at epoch: | 45380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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