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 48843U 26145.60586251 +.00000000 +00000-0 +37949-3 0 00006
2 48843 97.3339 222.1596 0005196 2.6527 357.4737 15.23072299 09
| Epoch (UTC): | 25 May 2026 14:32:26 |
| Eccentricity: | 0.0005196 |
| inclination: | 97.3339° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 222.1596° |
| argument of perigee: | 2.6527° |
| revolutions per day: | 15.23072299 |
| mean anomaly at epoch: | 357.4737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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