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 28413U 26150.49811256 +.00000000 +00000-0 +51640-3 0 00000
2 28413 97.5865 177.5581 0006194 181.4224 178.6993 15.17711769 04
| Epoch (UTC): | 30 May 2026 11:57:16 |
| Eccentricity: | 0.0006194 |
| inclination: | 97.5865° |
| perigee height: | 508 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 177.5581° |
| argument of perigee: | 181.4224° |
| revolutions per day: | 15.17711769 |
| mean anomaly at epoch: | 178.6993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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