▸Orbital parameters

Orbit class	LEO
Inclination	45.6172°
Eccentricity	0.0012429
Period	93.8 min
Apogee	468 km
Perigee	451 km
Mean motion	15.35492630 rev/day
RAAN	12.5895°
Arg of perigee	226.6423°
Mean anomaly	133.3438°
B*	2.8570e-4
Rev at epoch	12,481

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 59442U 24066A 26187.95466801 .00009748 00000-0 28570-3 0 9998

2 59442 45.6172 12.5895 0012429 226.6423 133.3438 15.35492630124813

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TSAT-1A",
  "OBJECT_ID": "2024-066A",
  "EPOCH": "2026-07-06T22:54:43.316+00:00",
  "MEAN_MOTION": 15.3549263,
  "ECCENTRICITY": 0.0012429,
  "INCLINATION": 45.6172,
  "RA_OF_ASC_NODE": 12.5895,
  "ARG_OF_PERICENTER": 226.6423,
  "MEAN_ANOMALY": 133.3438,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59442,
  "REV_AT_EPOCH": 12481,
  "BSTAR": 0.0002857,
  "MEAN_MOTION_DOT": 0.00009748,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	TSAT-1A
Operator	Tata Advanced Systems LtdHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Agency for Defense DevelopmentMEDIUMvia Wikidata
Country	India
Launch date	Apr 7, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	42HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/59442

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.