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 41948U 26064.62139019 +.00000000 +00000-0 +13693-4 0 00004
2 41948 97.4240 125.7921 0004193 237.7552 122.3276 15.19203388 02
| Epoch (UTC): | 05 March 2026 14:54:48 |
| Eccentricity: | 0.0004193 |
| inclination: | 97.4240° |
| perigee height: | 505 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 125.7921° |
| argument of perigee: | 237.7552° |
| revolutions per day: | 15.19203388 |
| mean anomaly at epoch: | 122.3276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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