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 48268U 26145.62976638 +.00000000 +00000-0 +12653-3 0 00006
2 48268 97.8938 220.7211 0001440 99.3700 260.7675 14.81669758 04
| Epoch (UTC): | 25 May 2026 15:06:51 |
| Eccentricity: | 0.0001440 |
| inclination: | 97.8938° |
| perigee height: | 623 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 220.7211° |
| argument of perigee: | 99.3700° |
| revolutions per day: | 14.81669758 |
| mean anomaly at epoch: | 260.7675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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