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 01459U 26091.58132292 +.00000000 +00000-0 +00000-0 0 00002
2 01459 41.4000 2.0993 4843830 90.5920 359.7322 0.21385678 09
| Epoch (UTC): | 01 April 2026 13:57:06 |
| Eccentricity: | 0.4843830 |
| inclination: | 41.4000° |
| perigee height: | 54526 km |
| apogee height: | 168956 km |
| right ascension of ascending node: | 2.0993° |
| argument of perigee: | 90.5920° |
| revolutions per day: | 0.21385678 |
| mean anomaly at epoch: | 359.7322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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