IRNSS 1I, 43286
Orbit data source: Space-Track
IRNSS 1I, 43286 is a payload satellite owned by ISRO (IN) in GEO that was launched on Wed, 11 Apr 2018 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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43286 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Operational Civil Navigation
Bus & Motor
I1K, ISRO LAM
Mass
1,425 kg wet, 598 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
6.961 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IRNSS 1I
1 43286U 18035A 26125.91689917 .00000090 00000-0 00000-0 0 9995
2 43286 29.0788 74.8480 0017662 186.9011 347.2974 1.00278576 29652Epoch: 2026-05-05T22:00Z
TLE epoch observation values (Epoch: 2026-05-05T22:00:20.088Z)
Latitude
2.79348°
Longitude
55.89158°
Altitude
35,711.223 km
Speed
3.08 km/s
True Right ascension
16h 39m 02s
True Declination
2° 47' 26"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:02:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,859.861 km
Perigee altitude
35,710.922 km
Semi-major axis
42,163.529 km
Eccentricity
0.00177
Inclination
29.0788°
RAAN
74.848°
Arg. of periapsis
186.9011°
True anomaly
347.2528°
Mean anomaly
347.2974°
Eccentric anomaly
347.27511°
Mean motion
0.25069 °/min
Orbital period
1,436.03 mins
BSTAR
0
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Other satellites on launch #35 in the year 2018 (2018-04-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRNSS 1I Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| IRNSS 1I is likely not visible in the next few days. |
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43286 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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