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 08874U 26088.18123396 +.00000000 +00000-0 +88557-4 0 00004
2 08874 82.9603 153.5563 0023485 348.6468 11.4155 13.75274498 03
| Epoch (UTC): | 29 March 2026 04:20:58 |
| Eccentricity: | 0.0023485 |
| inclination: | 82.9603° |
| perigee height: | 963 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 153.5563° |
| argument of perigee: | 348.6468° |
| revolutions per day: | 13.75274498 |
| mean anomaly at epoch: | 11.4155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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