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 08916U 26150.50988478 +.00000000 +00000-0 +00000-0 0 00000
2 08916 3.3945 269.0811 0003384 228.5265 328.2037 0.99473610 09
| Epoch (UTC): | 30 May 2026 12:14:14 |
| Eccentricity: | 0.0003384 |
| inclination: | 3.3945° |
| perigee height: | 35998 km |
| apogee height: | 36026 km |
| right ascension of ascending node: | 269.0811° |
| argument of perigee: | 228.5265° |
| revolutions per day: | 0.99473610 |
| mean anomaly at epoch: | 328.2037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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