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 is defined by the following mean orbital elements,
1 44619U 26024.76084532 +.00000000 +00000-0 +82725-3 0 00003
2 44619 98.3007 221.8878 0012410 331.7058 28.3490 15.02392983 02
| Epoch (UTC): | 24 January 2026 18:15:37 |
| Eccentricity: | 0.0012410 |
| inclination: | 98.3007° |
| perigee height: | 551 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 221.8878° |
| argument of perigee: | 331.7058° |
| revolutions per day: | 15.02392983 |
| mean anomaly at epoch: | 28.3490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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