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 36987U 99025EBT 24353.03314856 .00000864 00000-0 11356-2 0 9991
2 36987 100.8537 198.8447 0319984 179.1511 181.0225 13.45379945560391
| Epoch (UTC): | 18 December 2024 00:47:44 |
| Eccentricity: | 0.0319984 |
| inclination: | 100.8537° |
| perigee height: | 850 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 198.8447° |
| argument of perigee: | 179.1511° |
| revolutions per day: | 13.45379945 |
| mean anomaly at epoch: | 181.0225° |
| orbit number at epoch: | 56039 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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