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 03618U 26087.93703977 +.00000000 +00000-0 +34349-3 0 00005
2 03618 80.5304 264.4552 0083962 9.2677 143.6531 12.55899179 06
| Epoch (UTC): | 28 March 2026 22:29:20 |
| Eccentricity: | 0.0083962 |
| inclination: | 80.5304° |
| perigee height: | 1374 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 264.4552° |
| argument of perigee: | 9.2677° |
| revolutions per day: | 12.55899179 |
| mean anomaly at epoch: | 143.6531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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