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 25544U 98067A 24161.03725045 .00004252 00000-0 81357-4 0 9991
2 25544 51.6405 355.6642 0008363 274.3383 228.2512 15.50382241457283
Epoch (UTC):
| 09 June 2024 00:53:38
|
Eccentricity:
| 0.0008363
|
inclination:
| 51.6405
°
|
perigee height:
| 410 km
|
apogee height:
| 421 km
|
right ascension of ascending node:
| 355.6642
°
|
argument of perigee:
| 274.3383
°
|
revolutions per day:
| 15.50382241
|
mean anomaly at epoch:
| 228.2512
°
|
orbit number at epoch:
| 45728
|
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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