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 44794U 26144.05897169 +.00000000 +00000-0 +00000-0 0 00003
2 44794 53.9315 300.6372 0004812 48.4717 311.5477 1.86227499 09
| Epoch (UTC): | 24 May 2026 01:24:55 |
| Eccentricity: | 0.0004812 |
| inclination: | 53.9315° |
| perigee height: | 21515 km |
| apogee height: | 21542 km |
| right ascension of ascending node: | 300.6372° |
| argument of perigee: | 48.4717° |
| revolutions per day: | 1.86227499 |
| mean anomaly at epoch: | 311.5477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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