IRNSS 1F, 41384
Orbit data source: Space-Track
IRNSS 1F, 41384 is a payload satellite owned by ISRO (IN) in GEO that was launched on Thu, 10 Mar 2016 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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41384 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Partially 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 IRNSS 1F
1 41384U 16015A 26296.85392080 .00000175 00000-0 00000+0 0 9995
2 41384 5.6682 93.8327 0021443 174.6006 103.7513 1.00277876 38952Epoch: 2026-10-23T20:29Z
TLE epoch observation values (Epoch: 2026-10-23T20:29:38.757Z)
Latitude
-5.59155°
Longitude
32.7407°
Altitude
35,807.168 km
Speed
3.073 km/s
True Right ascension
00h 49m 40s
True Declination
-5° 35' 09"
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
21:42:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,876.355 km
Perigee altitude
35,695.53 km
Semi-major axis
42,164.08 km
Eccentricity
0.00214
Inclination
5.6682°
RAAN
93.8327°
Arg. of periapsis
174.6006°
True anomaly
103.98982°
Mean anomaly
103.7513°
Eccentric anomaly
103.87058°
Mean motion
0.25069 °/min
Orbital period
1,436.06 mins
BSTAR
0
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Other satellites on launch #15 in the year 2016 (2016-03-10 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 1F 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 1F is likely not visible in the next few days. |
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41384 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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