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 36827U 26104.14653389 +.00000000 +00000-0 +73751-4 0 00008
2 36827 98.4405 315.4954 0042281 66.1540 294.4074 14.44780348 01
| Epoch (UTC): | 14 April 2026 03:31:00 |
| Eccentricity: | 0.0042281 |
| inclination: | 98.4405° |
| perigee height: | 713 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 315.4954° |
| argument of perigee: | 66.1540° |
| revolutions per day: | 14.44780348 |
| mean anomaly at epoch: | 294.4074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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