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 48915U 26145.25294531 +.00000000 +00000-0 +21352-3 0 00005
2 48915 97.6999 330.7200 0006536 82.9205 277.2788 15.47976379 08
| Epoch (UTC): | 25 May 2026 06:04:14 |
| Eccentricity: | 0.0006536 |
| inclination: | 97.6999° |
| perigee height: | 418 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 330.7200° |
| argument of perigee: | 82.9205° |
| revolutions per day: | 15.47976379 |
| mean anomaly at epoch: | 277.2788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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